53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
20th AIAA/ASME/AHS Adaptive Structures Conference 14th AIAA Non-Deterministic Approaches Conference 13th AIAA Gossamer Systems Forum
23–26 April 2012
Sheraton Waikiki Honolulu, Hawaii
8th AIAA Multidisciplinary Design Optimization Specialist Conference
FINAL PROGRAM
Organizing Committees 53rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference GENERAL CHAIR Steven G. Russell Triumph Aerostructures TECHNICAL PROGRAM CHAIR Stephen B. Clay Air Force Research Laboratory STUDENT PAPERS TECHNICAL CHAIR Robert M. Taylor Lockheed Martin Aeronautics Company STRUCTURES TECHNICAL CHAIR David Wieland Southwest Research Institute STRUCTURAL DYNAMICS TECHNICAL CHAIR Jon Black Air Force Institute of Technology SURVIVABILITY TECHNICAL CHAIR Eric Fahrenthold University of Texas
20th AIAA/ASME/AHS Adaptive Structures Conference GENERAL CHAIR Edward V. White The Boeing Company TECHNICAL PROGRAM CHAIR David F. Voracek NASA Dryden Flight Research Center
14th AIAA NonDeterministic Approaches Conference GENERAL CHAIR Thiagarajan Krishnamurthy NASA Langley Research Center TECHNICAL PROGRAM CHAIR Gianluca Iaccarino Stanford University
13th AIAA Gossamer Systems Forum
Tweeting during the SDM Conference Use #AIAASDM
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GENERAL CHAIR Sergio Pellegrino California Institute of Technology TECHNICAL PROGRAM CHAIR James D. Moore ManTech Nexolve
MATERIALS TECHNICAL CHAIR Gary Seidel Virginia Tech
8th AIAA Multidisciplinary Design Optimization Specialist Conference
DESIGN ENGINEERING TECHNICAL CHAIR Brian Robbers Aerojet
GENERAL CHAIR Vladimir O. Balabanov The Boeing Company
ASME REPRESENTATIVE Greg Odegard Michigan Tech
Connect online with AIAA
TECHNICAL PROGRAM CHAIR Karen Willcox Massachusetts Institute of Technology
ASCE REPRESENTATIVE Wieslaw Binienda University of Akron
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Synopsis 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) Sponsored by AIAA, ASME, ASCE, AHS, and ASC, this established annual conference is a widely acknowledged event that provides a unique forum dedicated to the latest developments in the collective disciplines of structures, structural dynamics, materials, design engineering, and survivability. Plenary presentations by recognized, forward-thinking invited speakers will be a special feature of the conference. This year’s presentations will be organized around the potential applications of structures, structural dynamics, and materials in the next generation of aircraft. The 53rd Conference will also host:
The 20th AIAA/ASME/AHS Adaptive Structures Conference (ASC) Bringing together basic and applied researchers from diverse disciplines in academia, government, and industry, this is the premier conference focused on the advancement of adaptive structures technology and its application to aerospace systems.
The 14th AIAA Non-Deterministic Approaches Conference (NDA)
The 13th AIAA Gossamer Systems Forum (GSF) An emerging class of large-scale, lightweight structures is enabling a paradigm shift in design, launch, and operation of spaceflight systems. Spacecraft with structural characteristics optimized for operation in space and for the ability to collapse into small packages for launch yield order-ofmagnitude reductions in mass, launch volume, and life-cycle cost, as compared to large spaceflight systems.
The aerospace industry increasingly recognizes the need for non-deterministic approaches (NDA) to manage uncertainty. These approaches include both probabilistic and non-probabilistic methods, and provide treatment of high consequence of failure events associated with the development and operation of aerospace systems.
The 8th AIAA Multidisciplinary Design Optimization Specialist Conference (MDO) Multidisciplinary design optimization (MDO) focuses on optimizing the performance and reducing the costs of complex systems that involve multiple interacting disciplines, such as those found in aircraft, spacecraft, automobiles, industrial manufacturing equipment, and various consumer products, as well as on the development of related methodologies. MDO is a broad area that encompasses design synthesis, sensitivity analysis, approximation concepts, optimization methods and strategies, artificial intelligence, and rule-based design—all in the context of integrated design dealing with multiple disciplines, and interacting subsystems or systems of systems.
Special Events Monday, 23 April 2012
Wednesday, 25 April 2012
0800–0900 hrs SDM Keynote—Composites Safety and Certification Initiatives
0800–0900 hrs ASC Keynote—Adaptive Structures: The Journey to Flight
Larry Ilcewicz Chief Scientific and Technical Advisor for Advanced Composite Materials, Federal Aviation Administration, Renton, WA 1330–1430 hrs SDM Lecture—Tailoring of Composite Structures Using Spatially Varying
Fiber Orientations
Michael Hyer N. Waldo Harrison Professor Emeritus of Engineering Science and Mechanics, Virginia Polytechnic Institute and State University, Blacksburg, VA 1800–1930 hrs
Welcome Reception
Tuesday, 24 April 2012 0800–0900 hrs MDO Keynote—Multidisciplinary Design Optimization: What Remains
to Be Done
Natalia Alexandrov Senior Research Scientist, NASA Langley Research Center, Hampton, VA 1330–1430 hrs NDA Keynote—U ncertainty Quantification in System Risk Assessment
George A. Lesieutre Professor and Head, Aerospace Engineering, Pennsylvania State University, State College, PA 1200 hrs
Awards Luncheon David W. Trop Chief Engineer – Structures, Product Development and Technology, Boeing Commercial Airplanes, Seattle, WA 1800–1900 hrs ASME Adaptive Structures and Materials Systems Prize Lecture—
Adaptive Energy Absorption for Transportation Systems Using Magnetorheological Fluids Norman Werely University of Maryland, College Park, MD
Thursday, 26 April 2012 0800–0900 hrs GSF Keynote—Gossamer Systems for Satellite Deorbiting: The CUBESAIL
and DEORBITSAIL Space Missions
Vaios Lappas University of Surrey, Guildford, United Kingdom
and Decision-Making
Sankaran Mahadevan John R. Murray Sr. Chair in Engineering, Vanderbilt University, Nashville, TN 2
Conference Information Accompanying Persons Program Accompanying persons are invited to meet in room Regency II at the Royal Hawaiian Hotel for coffee at 1000 hrs on Monday, 23 April 2012. A representative from the Hawaii Convention & Visitors Bureau will be on hand to give a short talk about what is available to see and do in the area, as well as to answer any questions you have regarding tours, shopping, dining or anything else about Honolulu. In addition, the first 25 people to arrive will receive a ticket for a free lei making class immediately following the Accompanying Persons Program. Monday Welcome Reception 1800–1930 hrs Visit with your colleagues during the opening reception. Come enjoy local Hawaiian entertainment and foods, on the pool lawn. Tickets are included in your registration fee where indicated. Additional tickets may be purchased at the on-site registration desk for $85, based on availability. Wednesday Awards Luncheon 1200–1400 hrs Join fellow attendees on Wednesday, 25 April 2012, at the AIAA Awards Luncheon. The luncheon is included in the registration fee where indicated. Additional tickets may be purchased at the on-site registration desk for $48, based on availability. AWARDS TO BE PRESENTED INCLUDE: Aerospace Design Engineering Award Ronald Hughes, Principal Engineering Fellow (retired), Raytheon Combat Systems, Dallas, Texas “For demonstrated excellence in the design, integration, development and production of weapon system airframes and mechanical subsystems in missile systems, and for the promotion of disciplined design processes.” Walter J. and Angeline H. Crichlow Trust Prize Chin-Teh (C. T.) Sun, Neil Armstrong Distinguished Professor of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana “For pioneering developments in damage tolerant design in composite structural mechanics and for seminal contributions to academic programs in composite structures and materials.”
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Survivability Award Joel Williamsen, Task Leader, Live Fire Test and Evaluation, Institute for Defense Analyses Alexandria, Virginia “For enhancing spacecraft, aircraft, and crew survivability through advanced meteoroid/ orbital debris shield designs, on-orbit repair techniques, risk assessment tools, and Live Fire evaluation.” ASME/Boeing Best Paper Michael Lawson and Jayant Sirohi, University of Texas-Austin AIAA 2011-1876, “Measurement of Deformation of Rotating Blades Using Digital Image Correlation” Gossamer Systems Best Paper Hirotaka Sawada, Osamu Mori, Nobukatsu Okuizumi, Yoji Shirasawa, Japan Aerospace Exploration Agency; Yasuyuki Miyazaki, Nihon University; N. Natori, Waseda University; and Saburo Matunaga, Hiroshi Furuya, Hiraku Sakamoto, Tokyo Institute of Technology AIAA 2011-1887, “Mission Report on The Solar Power Sail Deployment Demonstration of IKAROS” Student Papers Awards A limited number of students will receive recognition for their papers at the SDM conference awards luncheon on Wednesday, 25 April 2012, through the Jefferson Goblet Award, The Harry H. and Lois G. Hilton Award, The Lockheed Martin Award, and The American Society for Composites Award. Speaker and Session Chair Information Session Chair Forms Session chairs are asked to complete a Session Chair Report for each session. This year we have moved to an electronic session chair form. Download the app on your smart phone or tablet or visit the reporting station and enter your session information. If you do not have a smart phone, simply fill out the form during your session and enter your results at the session chair reporting station, located at the registration desk. Reports are collected and used for planning purposes, including future session topics and room allocations. Please submit your session information electronically before the end of the conference.
“No Paper, No Podium” Policy If a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the conference. International Traffic in Arms Regulations (ITAR) AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance. Speakers’ Briefing Authors who are presenting papers will meet in the Maui Room for a short briefing with session chairs and co-chairs at 0700 hrs. Continental breakfast will be provided. When you arrive please sit at the table labeled with your session number (e.g., 1-SDM-1). Please be sure to wear your name badge and attend on the day of your session(s) only. Speakers’ Practice Speakers wishing to practice their presentations may do so in the Manor Wing Green Room. A sign-up sheet will be posted on the door. In consideration of others, please limit practice time to 30-minute increments. Timing of Presentations Each paper will be allotted 30 minutes (including introduction and question-andanswer period) except where noted. Audiovisual Each session room will be preset with one LCD projector and one screen. A 1/2", VHS VCR and monitor, an overhead projector, and/ or a 35-mm slide projector will be provided if requested by presenters on their abstract submittal forms. AIAA does not provide computers or technicians to connect LCD projectors to computers. Should presenters wish to use an LCD projector, it is their responsibility to bring or arrange for a computer on their own. Please note that AIAA does not provide security in the session rooms, and recommends that items of value, including computers, not be left unattended. Any additional audiovisual requirements requested on site will be at cost to the presenter. For additional A/V equipment, please visit the registration desk.
Conference Information continued Journal Publication Authors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Computing, Information, and Communication. You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa. Conference Proceedings This year’s conference proceedings will be available as online proceedings. This cost is included in the registration fee where indicated. If you register on site, you will be provided with instructions at registration. Online proceedings packages may be purchased separately at the registration desk for $170. Membership Professionals registering at the nonmember rate will receive a one-year AIAA membership.
30% Off All Books at SDM AIAA is offering a special discount on all titles, including children’s books, featured at SDM 2012. Attendees may take advantage of a 30% discount off the list price of all books for sale at the AIAA bookstore. This special will only be available during SDM. In addition, AIAA will be featuring Design and Analysis of Composite Structures; with Applications to Aerospace Structures, by Christos Kassapoglou, at a 35% discount. A limited number of books are available at these prices, so make it a point to stop by the bookstore while you are at SDM. Employment Opportunities AIAA assists members who are searching for employment by providing a bulletin board at technical meetings. This bulletin board is solely for “open position” and “available for employment” postings. Employers are encouraged to have personnel who are attending an AIAA technical conference to bring “open position” job postings. Individual AIAA members may post “available for employment” notices. AIAA cannot assume responsibility for notices forwarded to AIAA
Headquarters. AIAA reserves the right to remove inappropriate notices. AIAA members may post resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter.aiaa.org. Conference Certificate of Attendance Available Certificates of Attendance are available for attendees who request documentation at the time of the conference. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant. Please request your copy at the on-site registration desk. Restrictions Video or audio recording of sessions, as well as the unauthorized sale of AIAA copyrighted material, is prohibited.
REGISTRATION AND INFORMATION CENTER HOURS Registration and Bookstore Hours Sunday, 22 April
1500–1900 hrs
Monday, 23 April
0700–1700 hrs
Tuesday, 24 April
0700–1700 hrs
Wednesday, 25 April 0700–1700 hrs Thursday, 26 April 0700–1700 hrs
Cyber Café Hours
Networking Breaks
There will be computers with complimentary Internet access located in the foyer.
Grab a cup of coffee and network with your fellow conference attendees in the foyer.
Sunday, 22 April
1500–2000 hrs
Monday, 23 April
0700–2000 hrs
Tuesday, 24 April
0700–2000 hrs
Wednesday, 25 April 0700–2000 hrs Thursday, 26 April 0700–1700 hrs
Monday, 23 April
0900–0930 hrs 1430–1500 hrs
Tuesday, 24 April
0900–0930 hrs 1430–1500 hrs
Wednesday, 25 April 0900–0930 hrs 1400–1430 hrs Thursday, 26 April 0900–0930 hrs
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Technical and Program Committee Organizational Chart
and 14 Program Committees
• Aerospace Design and Structures Adaptive Structures Design Engineering Materials Multidisciplinary Design Optimization Non-Deterministic Approaches Structural Dynamics Structures Survivability
(PCs). Technical committees
• Aerospace Sciences
The Technical Activities Committee (TAC), led by AIAA’s Vice President for Technical Activities, is responsible for overseeing the operation of AIAA’s 69 Technical Committees (TCs)
are organized into seven Technical Groups, each of which is led by a Technical Director. These groups include Aerospace Design and Structures; Aerospace Sciences; Aircraft and Atmospheric Systems; Engineering and Technology Management; Information Systems; Propulsion and Energy; and Space and Missiles. AIAA TCs and PCs are a great way to get engaged, expand one’s professional network, and help the Institute deliver quality products and services to the aerospace community. AIAA TCs and PCs are responsible for many aspects of the activities of the Institute, including conducting the many technical discipline and systems conferences, recognizing technical excellence through awards, generating standards, and presenting short courses. For more information about AIAA’s Technical and Program Committees, please visit www.aiaa.org/committees
Aeroacoustics Aerodynamic Measurement Technology Applied Aerodynamics Astrodynamics Atmospheric and Space Environments Atmospheric Flight Mechanics Fluid Dynamics Ground Testing Guidance, Navigation, and Control Meshing, Visualization, and Computational Environments Modeling and Simulation Plasmadynamics and Lasers Thermophysics
• Aircraft and Atmospheric Systems Aerodynamic Decelerator Systems Aircraft Design Aircraft Operations Air Transportation Systems Balloon Systems Flight Testing General Aviation Lighter-Than-Air Systems Product Support V/STOL Aircraft Systems • E ngineering and Technology Management Economics History Legal Aspects of Aeronautics and Astronautics Management Society and Aerospace Technology Systems Engineering • Information Systems Communications Systems Computer Systems Digital Avionics Information and Command and Control Systems Intelligent Systems Sensor Systems
• Propulsion and Energy Aerospace Power Systems Air Breathing Propulsion Systems Integration Electric Propulsion Energetic Components and Systems Gas Turbine Engines High Speed Air Breathing Propulsion Hybrid Rockets Liquid Propulsion Nuclear and Future Flight Propulsion Propellants and Combustion Solid Rockets Terrestrial Energy Systems • Space and Missiles Life Sciences and Systems Microgravity and Space Processes Missile Systems Space Architecture Space Automation and Robotics Space Colonization Space Logistics Space Operations and Support Space Resources Space Systems Space Tethers Space Transportation Weapon System Effectiveness • Program Committees Aerospace Traffic Management Directed Energy Systems Energy Optimized Aircraft and Equipment Systems Gossamer Spacecraft Green Engineering Homeland Security HyTASP Netcentric Operations Reusable Launch Vehicles Space Environmental Systems Space Exploration Space Station Unmanned Systems Value Driven Design
Software 5
Technical Committee and Other Meetings Time
Location
Saturday, 21 April 2012 0800–1800 hrs Aeroelastic Prediction Workshop
Kauai & Honolulu
Sunday, 22 April 2012 0800–1800 hrs Aeroelastic Prediction Workshop
Kauai & Honolulu
1830–2200 hrs Structures TC
Kahuku
Monday, 23 April 2012 1000–1100 hrs Accompanying Persons Program
Regency II (Royal Hawaiian) **
1130–1330 hrs Aerospace Design and Structures Group Meeting
Regency I (Royal Hawaiian) **
1900–2100 hrs Survivability TC
Honolulu
1900–2200 hrs ASME Structures and Materials Technical Committee
Kona
Tuesday, 24 April 2012 0800–1200 hrs DETC Subcommittee
Regency I (Royal Hawaiian) **
1200–1330 hrs SDM Long Range Planning Meeting
Regency II (Royal Hawaiian) **
1900–2200 hrs AIAA Adaptive Structures TC
Oahu/Waialua
1900–2200 hrs Design Engineering TC
Kona
1900–2230 hrs AIAA Materials TC
Waianae
1900–2200 hrs AIAA Multidisciplinary Design Optimization TC
Maui
1900–2200 hrs AIAA Non-Deterministic Approaches TC
Honolulu/Kahuku
1900–2200 hrs AIAA Structures TC
Molokai
1900–2200 hrs AIAA Structural Dynamics TC
Lanai
Wednesday, 25 April 2012 1730–1900 hrs SDM 2013 Planning Meeting
Maui
1830–1930 hrs Crichlow Trust Prize Reception (invitation only)
Honolulu
1900–2200 hrs AIAA Gossamer Spacecraft PC
Oahu/Waialua
Thursday, 26 April 2012 1200–1300 hrs SDM Strategic Direction Committee
Regency II (Royal Hawaiian) **
** Royal Hawaiian is the pink hotel next door to the Sheraton Waikiki
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Sessions at a Glance Session ID-Abbreviation
Session Title
Start Time
Location
Monday 01-SDM-01
SDM Keynote: Composites Safety and Certification Initiatives
0800 hrs
Kauai
02-MDO-01
Optimization Applications I
0930 hrs
Hilo
03-MDO-02
Topology Optimization
0930 hrs
Niihau
04-NDA-01
Non-Deterministic Approaches to Structural Health Management I
0930 hrs
Honolulu
05-NDA-02
Uncertainty Quantification in Verification and Validation I
0930 hrs
Kauai
06-SDM-02
Plates and Panels
0930 hrs
Koko Crater
07-SDM-03
Impact Damage
0930 hrs
Lanai
08-SDM-04
Special Session I in Honor of Professor Michael W. Hyer
0930 hrs
Oahu
09-SDM-05
Fatigue and Fracture Mechanics I
0930 hrs
Kona
10-SDM-06
Dynamics of Composites
0930 hrs
Molokai
11-SDM-07
Space Structures Dynamics
0930 hrs
Puna
12-SDM-08
Turbine Blade Dynamics
0930 hrs
Akaka Falls
13-SDM-09
Air Vehicle Structural Dynamics I
0930 hrs
Waialua
14-SDM-10
Integrated Computational Materials Engineering (ICME) I
0930 hrs
Kohala
15-SDM-11
Nanostructured Materials I
0930 hrs
Waimea Canyon
16-SDM-12
Wind Turbine Structural Dynamics
0930 hrs
Kahuku
17-SDM-13
Wind Turbine Composite Material Analysis
0930 hrs
Waianae
18-SDM-14
SDM Lecture: Tailoring of Composite Structures Using Spatially Varying Fiber Orientations
1330 hrs
Kauai
19-MDO-03
Aeroelastic and Aerodynamic Optimization
1500 hrs
Puna
20-MDO-04
Design and Optimization Under Uncertainty
1500 hrs
Hilo
21-NDA-03
Non-Deterministic Approaches to Structural Health Management II
1500 hrs
Honolulu
22-NDA-04
Uncertainty Quantification in Verification and Validation II
1500 hrs
Kauai
23-SDM-15
Design
1500 hrs
Oahu
24-SDM-16
Structural Joints
1500 hrs
Waianae
25-SDM-17
Aeroelasticity and Flutter
1500 hrs
Lanai
26-SDM-18
Buckling of Composites
1500 hrs
Waialua
27-SDM-19
Aeroelastic Testing
1500 hrs
Molokai
28-SDM-20
Plate and Shell Dynamics
1500 hrs
Koko Crater
29-SDM-21
RotorCraft Dynamics
1500 hrs
Akaka Falls
30-SDM-22
Controls
1500 hrs
Waimea Canyon
31-SDM-23
Integrated Computational Materials Engineering (ICME) II
1500 hrs
Kohala
32-SDM-24
Hybrid Materials for Hypersonic Vehicles (MURI)
1500 hrs
Niihau
33-SDM-25
Wind Turbine Blade Design, Analysis, and Optimization
1500 hrs
Kahuku
34-SDM-26
Air and Space Survivability
1500 hrs
Kona
35-RCTP-01
Reception
1800 hrs
Poolside
36-MDO-05
MDO Keynote: Multidisciplinary Design Optimization: What Remains to be Done
0800 hrs
Kauai
37-ASC-01
Aerospace System Applications I
0930 hrs
Lanai
38-GSF-01
Inflatable Structures
0930 hrs
Honolulu
Tuesday
7
Sessions at a Glance Session ID-Abbreviation
Session Title
Start Time
Location
39-MDO-06
Optimization of Composites
0930 hrs
Puna
40-MDO-07
Optimization Applications II
0930 hrs
Hilo
41-NDA-05
Integrated Computational Materials Engineering (ICME) III
0930 hrs
Kauai
42-SDM-27
Structural and Thermal Interactions of Aerospace Systems
0930 hrs
Kona
43-SDM-28
Fatigue and Fracture of Composites
0930 hrs
Waianae
44-SDM-29
Fatigue and Fracture Mechanics II
0930 hrs
Waialua
45-SDM-30
Special Session II in Honor of Professor Michael W. Hyer
0930 hrs
Oahu
46-SDM-31
Aerothermal Dynamics
0930 hrs
Akaka Falls
47-SDM-32
Semi-Span Supersonic Transport
0930 hrs
Molokai
48-SDM-33
Air Vehicle Structural Dynamics II
0930 hrs
Niihau
49-SDM-34
Computational Aeroelasticity I
0930 hrs
Koko Crater
50-SDM-35
Nanostructured Materials II
0930 hrs
Waimea Canyon
51-SDM-36
Composite Processes and Characterization
0930 hrs
Kohala
52-SDM-37
Wind Turbine Composite Material Testing
0930 hrs
Kahuku
53-NDA-06
NDA Keynote: Uncertainty Quantification in System Risk Assessment and Decision-Making
1330 hrs
Kauai
54-ASC-02
Composite Structures Applications
1500 hrs
Oahu
55-GSF-02
Novel Applications and Innovations
1500 hrs
Honolulu
56-MDO-08
Special Session: MDO Past, Present, Future
1500 hrs
Niihau
57-NDA-07
Failure Analysis and Realability Assessment
1500 hrs
Hilo
58-NDA-08
Engineering Applications of Non-Deterministic Approaches I
1500 hrs
Kauai
59-SDM-38
Shells and Pressure Vessels
1500 hrs
Kona
60-SDM-39
Aircraft Design
1500 hrs
Waimea Canyon
61-SDM-40
Composite Damage and Delamination
1500 hrs
Waianae
62-SDM-41
Mesh Dependence of Failure Predictions
1500 hrs
Lanai
63-SDM-42
VibroAcoustics
1500 hrs
Koko Crater
64-SDM-43
Aeroelasticity I
1500 hrs
Akaka Falls
65-SDM-44
Micro Air Vehicle Aeroelastics
1500 hrs
Waialua
66-SDM-45
Damping and Vibration Supression
1500 hrs
Molokai
67-SDM-46
Multifunctional Materials
1500 hrs
Kohala
68-SDM-47
Multiscale Modeling of Damage in Composites
1500 hrs
Maui
69-SDM-48
Non-Deterministic Approaches Applied to Wind Energy
1500 hrs
Kahuku
70-SDM-49
Design Engineering
1500 hrs
Puna
71-ASC-03
ASC Keynote: Adaptive Structures: The Journey to Flight
0800 hrs
Kauai
72-ASC-04
Rotorcraft Applications
0930 hrs
Oahu
73-GSF-03
Deployable Apertures – Optics
0930 hrs
Honolulu
74-MDO-09
Optimization Frameworks
0930 hrs
Hilo
75-MDO-10
Optimization Methods
0930 hrs
Niihau
76-NDA-09
Development of Non-Deterministic Methods I
0930 hrs
Kauai
77-SDM-50
Developing the Next Generation of Shell Buckling Design Factors and Technologies I – Testing
0930 hrs
Lanai
Wednesday
8
Sessions at a Glance Session ID-Abbreviation
Session Title
Start Time
Location
78-SDM-51
Failure Analysis and Prediction I
0930 hrs
Waianae
79-SDM-52
Fatigue and Fracture Mechanics III
0930 hrs
Waialua
80-SDM-53
Sandwich Structures
0930 hrs
Kona
81-SDM-54
Flutter I
0930 hrs
Molokai
82-SDM-55
Beam Dynamics I
0930 hrs
Akaka Falls
83-SDM-56
Computational Aeroelasticity II
0930 hrs
Koko Crater
84-SDM-57
Design, Micro/Unmanned Aircraft
0930 hrs
Puna
85-SDM-58
Nanostructured Materials III
0930 hrs
Waimea Canyon
86-SDM-59
Fatigue and Creep in Materials
0930 hrs
Kohala
87-SDM-60
Wind Turbine Dynamics, Loads, and Control
0930 hrs
Kahuku
88-LNCH-01
Awards Luncheon
1200 hrs
Maui
89-ASC-05
Analysis and Design
1430 hrs
Kauai
90-GSF-04
Solar Sails
1430 hrs
Honolulu
91-MDO-11
Structural Optimization
1430 hrs
Niihau
92-MDO-12
Aircraft Optimization
1430 hrs
Hilo
93-NDA-10
Non-Deterministic Approaches for Aerospace Systems I
1430 hrs
Oahu
94-SDM-61
Composites Structures
1430 hrs
Waianae
95-SDM-62
Test and Analysis
1430 hrs
Kona
96-SDM-63
STS-133/ET-137 Intertank Stringer Cracks
1430 hrs
Lanai
97-SDM-64
Health Monitoring
1430 hrs
Waialua
98-SDM-65
Nonlinear Dynamics and Aeroelasticity I
1430 hrs
Koko Crater
99-SDM-66
Flutter II
1430 hrs
Molokai
100-SDM-67
Aeroelasticity II
1430 hrs
Akaka Falls
101-SDM-68
Design Process
1430 hrs
Puna
102-SDM-69
The Digital Twin Concept
1430 hrs
Kohala
103-SDM-70
Nanostructured Materials IV
1430 hrs
Waimea Canyon
104-SDM-71
Wind Turbine Aeroelasticity
1430 hrs
Kahuku
105-ASME-01
ASME Adaptive Structures and Materials Systems Prize Lecture
1800 hrs
Kauai
106-GSF-05
GSF Keynote: Gossamer Systems for Satellite Deorbiting: The CUBESAIL and DEORBITSAIL Space Missions
0800 hrs
Kauai
107-ASC-06
Systems and System Designs
0930 hrs
Kona
108-GSF-06
Deployable Apertures – RF
0930 hrs
Honolulu
109-MDO-13
Aircraft/Engine Optimization
0930 hrs
Hilo
110-MDO-14
Multi-Objective and Multi-Level Optimization Methods
0930 hrs
Niihau
111-NDA-11
Development of Non-Deterministic Methods II
0930 hrs
Kahuku
112-NDA-12
Non-Deterministic Approaches for Aerospace Systems II
0930 hrs
Oahu
113-SDM-72
Failure Analysis and Prediction II
0930 hrs
Waianae
114-SDM-73
Developing the Next Generation of Shell Buckling Design Factors and Technologies II – Analysis and Design Technology
0930 hrs
Lanai
115-SDM-74
Beam Analysis
0930 hrs
Waimea Canyon
116-SDM-75
Beam Dynamics II
0930 hrs
Molokai
Thursday
9
Sessions at a Glance Session ID-Abbreviation
Session Title
Start Time
Location
117-SDM-76
Impact Dynamics
0930 hrs
Akaka Falls
118-SDM-77
Experimental Dynamics Techniques
0930 hrs
Waialua
119-SDM-78
Dynamics of Fuel Slosh and Tanks
0930 hrs
Koko Crater
120-SDM-79
Design, Composite Structures
0930 hrs
Puna
121-SDM-80
Characterization of Composite Materials
0930 hrs
Kohala
122-SDM-81
Aerospace Materials Applications
0930 hrs
Kauai
123-ASC-07
Aerospace System Applications II
1300 hrs
Kauai
124-GSF-07
Materials and Testing
1300 hrs
Kona
125-GSF-08
Wrinkling and Non-Linear Effects
1300 hrs
Hilo
126-MDO-15
Aerostructural and Aeroelastic Optimization
1300 hrs
Maui
127-MDO-16
Surrogate-based and Multi-fidelity Optimization Methods
1300 hrs
Niihau
128-NDA-13
Non-Deterministic Design and Optimization
1300 hrs
Kahuku
129-NDA-14
Engineering Applications of Non-Deterministic Approaches II
1300 hrs
Oahu
130-SDM-82
Composites Modeling
1300 hrs
Waianae
131-SDM-83
Deployable Structures
1300 hrs
Lanai
132-SDM-84
Buckling
1300 hrs
Honolulu
133-SDM-85
Modeling
1300 hrs
Waimea Canyon
134-SDM-86
Nonlinear Dynamics
1300 hrs
Molokai
135-SDM-87
Nonlinear Dynamics and Aeroelasticity II
1300 hrs
Koko Crater
136-SDM-88
Dynamics of Micro-Aircraft
1300 hrs
Waialua
137-SDM-89
Modeling and Simulation
1300 hrs
Akaka Falls
138-SDM-90
Design, Advanced Aircraft
1300 hrs
Puna
139-SDM-91
Materials Model Development and Applications
1300 hrs
Kohala
10
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Committee Meetings
Registration Open
Tuesday
www.aiaa.org/events/sdm
Committee Meetings
Opening Reception
Committee Meetings
Technical Sessions
Networking Coffee Break
Networking Coffee Break
Technical Sessions
NDA Keynote
Lunch Break
SDM Lecture
Lunch Break
Technical Sessions
Networking Coffee Break
Networking Coffee Break
Technical Sessions
MDO Keynote
Speakers’ Breakfast
24 April 2012
SDM Keynote
Speakers' Breakfast
Monday 23 April 2012
Sunday
22 April 2012
Committee Meetings
ASME Lecture
Technical Sessions
Networking Coffee Break
Awards Luncheon
Technical Sessions
Networking Coffee Break
ASC Keynote
Speakers’ Breakfast
25 April 2012
Wednesday
www.aiaa.org/events/sdm
Technical Sessions
Lunch Break
Technical Sessions
Networking Coffee Break
GSF Keynote
Speakers’ Breakfast
26 April 2012
Thursday
Event at a Glance
Sheraton Waikiki Floor Plan
12
13
S. Lee, H. Lee, Hanyang University, Seoul, B. Stanford, P. Beran, Air Force Research South Korea; G. Park, Hanyang University, Laboratory, Wright-Patterson AFB, OH; M. Ansan City, South Korea Kobayashi, University of Hawaii, Manoa, Honolulu, HI
S. Chowdhury, J. Zhang, M. Catalano, Rensselaer Polytechnic Institute, Troy, NY; A. Messac, Syracuse University, Syracuse, NY; L. Castillo, Texas Tech University, Lubbock, TX
1030 hrs AIAA-2012-1352 Exploring the Best Performing Commercial Wind Turbines for Different Wind Regimes in a Target Market
M. Gobbato, J. Kosmatka, J. Conte, University of California, San Diego, La Jolla, CA
T. Krishnamurthy, NASA Langley Research Center, Hampton, VA; A. Gallegos, Lockheed Martin Corporation, Hampton, VA
1130 hrs AIAA-2012-1354 Hybrid Optimization for Wind Turbine Thick Airfoils
1130 hrs AIAA-2012-1359 Parameterization of Curvilinear Spars and Ribs (SpaRibs) for Optimum Wing Structural Design
A. Verbart, National Aerospace Laboratory D. Locatelli, S. Mulani, R. Kapania, Virginia (NLR), Amsterdam, The Netherlands; M. Polytechnic Institute and State University, Langelaar, N. van Dijk, F. Van Keulen, Blacksburg, VA Delft University of Technology, Delft, The Netherlands
1100 hrs AIAA-2012-1358 Level Set Based Topology Optimization with Stress Constraints and Consistent Sensitivity Analysis
Topology Optimization
F. Grasso, Energy Research Center of the G. Fischer, A. Savill, T. Kipouros, Cranfield Netherlands, Petten, The Netherlands University, Cranfield, United Kingdom
1100 hrs AIAA-2012-1353 Multi-objective Shape Optimisation for Horizontal-Axis Wind Turbine Blades
Optimization Applications I
1130 hrs AIAA-2012-1364 Accounting for Proof Test Data in a Reliability Based Design Optimization Framework
S. Das, State University of New York, Buffalo, G. Venter, Stellenbosch University, Buffalo, NY; J. Spall, Johns Hopkins University Stellenbosch, South Africa; S. Scotti, NASA Applied Physics Laboratory, Laurel, MD; R. Langley Research Center, Hampton, VA Ghanem, University of Southern California, Los Angeles, CA
1100 hrs AIAA-2012-1363 Sensor configuration and optimization for identification of micro-anomalies in structural materials
Non-Deterministic Approaches to Structural Health Management I
Chaired by: R. ROSS, NASA Langley Research Center and E. TUEGEL, U.S Air Force 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1361 AIAA-2012-1362 AIAA-2012-1360 Damage Characterization Method for Dynamic Bayes Nets in SHM A Recursive Approach for Remaining Fatigue Life Predictions Structural Health Management Using G. Bartram, S. Mahadevan, Vanderbilt University, Nashville, TN Reduced Number of Sensor Inputs of Monitored Structural Systems
Monday, 23 April 2012 4-NDA-1
P. Kanakasabai, University of Wisconsin, Milwaukee, Milwaukee, WI
Opening Keynote Composites Safety and Certification Initiatives Dr. Larry Ilcewicz Chief Scientific and Technical Advisor for Advanced Composite Materials Federal Aviation Administration, Renton, WA
Chaired by: A. SUBRAMANIYAN, General Electric Company and J. DIAZ, University of La Coruna 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1356 AIAA-2012-1357 AIAA-2012-1355 Nonlinear Dynamic Response Simultaneous Topology Optimization A Deterministic Approach for Topology Optimization Using the of Membrane Wings and Their Reliability Based Topology Equivalent Static Loads Method Compliant Flapping Mechanisms Optimization
Monday, 23 April 2012 3-MDO-2
Technology, Atlanta, GA; R. Lepsch, NASA T. Jorris, S. Rexius, R. Carr, K. Bull, Hypersonic Combined Test Force, Edwards Langley Research Center, Hampton, VA AFB, CA; F. Friedl, E. Paulson, Air Force Research Laboratory, Edwards AFB, CA
Chaired by: J. WU, The Boeing Company 0930 hrs 1000 hrs AIAA-2012-1350 AIAA-2012-1351 Multidisciplinary Design MPD Augmentation of a Thermal Optimization for a Reusable Launch Air Rocket Utilizing Low Energy Vehicle Using Multiple-Phase Nuclear Reactions M. Fischer, A. Wilhite, Georgia Institute of Pseudospectral Optimization
Monday, 23 April 2012 2-MDO-1
Monday, 23 April 2012 1-SDM-1 0800 - 0900 hrs
Monday
Honolulu
Niihau
Hilo
Kauai
14
University, Nashville, TN
D. Quinn, A. Murphy, M. Price, Queen’s University Belfast, Belfast, United Kingdom Kalamazoo, MI
United Kingdom
L. Demasi, San Diego State University, San C. Bisagni, R. Vescovini, Technical Diego, CA; A. Palazotto, A. Hollenbeck, Air University of Milan, Milan, Italy Force Institute of Technology, Dayton, OH
R. Hart, University of Iowa, Iowa City, Iowa City, IA; O. Zhupanska,
1100 hrs AIAA-2012-1381 Characterization of Carbon Fiber Polymer Matrix Composites Subjected to Simultaneous Application of Electric Current Pulse and Low Velocity Impact
H. Cebeci, R. Guzman de Villoria, Massachusetts Institute of Technology, Cambridge, MA; K. Schulte, Technical University Hamburg, Hamburg, Germany; R. Jones, Virginia Polytechnic Institute and State University, Blacksburg, VA; B. Wardle, Massachusetts Institute of Technology, Cambridge, MA
1130 hrs AIAA-2012-1382 Effective Stiffness of Wavy Aligned Carbon Nanotubes for Modeling of Controlled-Morphology Polymer Nanocomposites
Special Session I in Honor of Professor Michael W. Hyer
J. Rhymer, H. Kim, University of California, S. Nguyen, E. Greenhalgh, J. Graham, A. San Diego, La Jolla, CA Francis, Imperial College London, London, United Kingdom
Chaired by: T. OCHINERO, Structural Mechanics Corporation and M. SCHULTZ, NASA Langley Research Center 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1379 AIAA-2012-1380 AIAA-2012-1378 Exploratory Structural Investigation Dynamic analysis of composite Developments in Morphing of a Hawkmoth-Inspired MAV’s stiffened panels subjected to Composites P. Weaver, University of Bristol, Bristol, Thorax compressive load
Monday, 23 April 2012 8-SDM-4
P. Akangah, K. Shivakumar, North Carolina C. Sika, D. Jensen, D. Allen, Brigham Young A&T State University, Greensboro, NC University, Provo, UT; C. Garvin, Novatek, Provo, UT; M. Jensen, Altus Poles, Provo, UT
M. Banker, National Aerospace Laboratories, Bangalore, India; D. Harursampath, N. Naik, Indian Institute of Science, Bangalore, India
1130 hrs AIAA-2012-1373 Efficient Stiffened Composite Plate Analysis
1100 hrs AIAA-2012-1377 Methodology for Predicting the Threat of Runway Debris Impact to Large Transport Aircraft
Impact Damage
F. Luraghi, ONERA, Toulouse, France
Plates and Panels
A. Urbina, M. Ross, Sandia National Laboratories, Albuquerque, NM; T. Paez, Thomas Paez Consulting, Durango, CO
1100 hrs AIAA-2012-1372 Efficient Design Optimization of Tow-Placed Panels for Enhanced Load-Carrying Capabilities by P. Gustafson, Western Michigan University, Adaptive Metamodeling
1030 hrs AIAA-2012-1371 Comparison of Stress and Strain Based Iteration for Fiber Tailoring of Bolted Composite Plates
Vanderbilt University, Nashville, TN
Chaired by: M. RASSAIAN, The Boeing Company and J. HUNT, Naval Air Systems Command 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1374 AIAA-2012-1375 AIAA-2012-1376 Impact Damage Resistance and Compression Strength After Impact Damage Prediction of Quasi-Isotropic Tolerance of Polymer Nanofiber of Unidirectional Fiberglass Rods Carbon/Epoxy Composite Panels Interleaved Composite Laminates Consolidated with Aramid Sleeves Impacted by High Velocity Ice
Monday, 23 April 2012 7-SDM-3
D. Kennedy, Cardiff University, Cardiff, United Kingdom; C. York, University of Glasgow, Glasgow, United Kingdom
Chaired by: V. GOYAL and G. HENSON, Invariant Laboratories 0930 hrs 1000 hrs AIAA-2012-1369 AIAA-2012-1370 Application of Quasi-Homogeneous The Impact of Composite Ply Anisotropic Laminates in GridContinuity Constraints on Aerospace stiffened Panel Design Stiffened Panel Design
Monday, 23 April 2012 6-SDM-2
B. Antoun, G. Wellman, F. Dempsey, V. Romero, Sandia National Laboratories, Albuquerque, NM
1100 hrs AIAA-2012-1368 Assessment of the Accuracy of a Model for Use in Prediction of Component Environments
Uncertainty Quantification in Verification and Validation I
Chaired by: B. THACKER, Southwest Research Institue and G. IACCARINO, Stanford University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1365 AIAA-2012-1366 AIAA-2012-1367 Comprehensive Framework A Method for Projecting Uncertainty Interpretations, relationships, and application issues in model for Integration of Calibration, from Sparse Samples of Discrete validation Verification and Validation Random Functions: Example of Y. Ling, S. Mahadevan, Vanderbilt S. Sankararaman, S. Mahadevan, Multiple Stress-Strain Curves
Monday, 23 April 2012 5-NDA-2
Oahu
Lanai
Koko Crater
Kauai
15
W. Yu, H. Pollayi, Utah State University, Logan, UT; D. Harursampath, Indian Institute of Science, Bangalore, India
1000 hrs AIAA-2012-1388 Evaluation of Strength of Component-Laminates in Stripbased Mechanisms
R. Maasha, NASA Marshall Space Flight Center, Huntsville, AL; R. Towner, Jacobs, Huntsville, AL
N. Yamamoto, R. Thevamaran, C. Daraio, California Institute of Technology, Pasadena, CA
1030 hrs AIAA-2012-1389 Dynamic Behavior of Periodic Structures Consisting of Vertically Aligned Carbon Nanotubes and Rigid Interlayers
1000 hrs AIAA-2012-1398 Temporal Life Prediction Analysis of a Turbine Engine Blade to Disk Attachment
1030 hrs AIAA-2012-1399 System identification of a reduced scale model blade with an Adaptive Pitch Link using whirl tower test data
1100 hrs AIAA-2012-1400 Comparison of Wind Turbine Models Subjected to Wind and Earthquake Loading
Turbine Blade Dynamics
J. Footdale, LoadPath, Albuquerque, NM; S. Jeon, CSA Engineering, Albuquerque, NM; T. Murphey, Air Force Research Laboratory, Kirtland AFB, NM
1100 hrs AIAA-2012-1395 Static Shape and Modal Testing of a Deployable Tensioned Phased Array Antenna
Space Structures Dynamics
H. Hu, H. Peng, National Cheng Kung University, Tainan, Taiwan
1100 hrs AIAA-2012-1390 Optimization of Axially Compressed Laminated Curved Panels with Cutouts
Dynamics of Composites
S. Naboulsi, P. Golden, Air Force Research C. Grappasonni, G. Coppotelli, University of A. Quilligan, A. O’Connor, Trinity College Laboratory, Wright-Patterson AFB, OH Rome “La Sapienza”, Rome, Italy; F. Nitzsche, Dublin, Dublin, Ireland A. Brown, P. Schmauch, NASA Marshall Carleton University, Ottawa, Canada Space Flight Center, Huntsville, AL; E. Lee, Jacobs, Huntsville, AL
Chaired by: A. BROWN 0930 hrs AIAA-2012-1397 Characterization of Deficiencies in the Frequency Domain Forced Response Analysis Technique for Turbine Bladed-Disks
Monday, 23 April 2012 12-SDM-8
Laboratory, California Institute of Dakota School of Mines & Technology, Technology, Pasadena, CA; G. Antoun, J. Rapid City, SD Tippmann, ATA Engineering, San Diego, CA
Chaired by: D. JOHNSON, NASA Glenn Research Center and Y. CHUNG, The Boeing Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1392 AIAA-2012-1393 AIAA-2012-1394 Analysis and Test Validation to Iterative Time Reversal in Correlation Results for a Mass Develop Mars Science Laboratory Dispersive and Non-Dispersive Loaded Vehicle Panel Test Article EDL Loads - Mobility Deploy Event Media Finite Element Models and Modal C. White, C. Peng, S. Lih, Jet Propulsion B. Fehrman, U. Korde, A. Cushman, South Survey Tests
Monday, 23 April 2012 11-SDM-7
K. Nadella, C. Cesnik, University of Michigan, Ann Arbor, Ann Arbor, MI; K. Salas, General Electric Company, Niskayuna, NY
Chaired by: J. BAND 0930 hrs AIAA-2012-1387 Characterization of Guided Wave Propagation in Composite Sandwich Structures
Monday, 23 April 2012 10-SDM-6
Technical Data Analysis, Inc., Falls Church, A. Arcari, N. Iyyer, Technical Data Analysis, VA; N. Phan, P. Kang, Naval Air Systems Inc., Falls Church, VA; M. Dunn, Naval Air Command, Patuxent River, MD Systems Command, Patuxent River, MD
C. Herrera, A. Harding, NASA Dryden Flight Research Center, Edwards, CA
1130 hrs AIAA-2012-1396 Orion Pad Abort 1 Crew Module Mass Properties Test Approach and Results
N. Mauch, Q. Zuo, University of Alabama, Huntsville, Huntsville, AL
1130 hrs AIAA-2012-1391 Effects of Engine Thrust, Mass, and Material Anisotropy on Flutter of a Composite Wing
1100 hrs AIAA-2012-1386 Effects of Surface Renewal on Fatigue Crack Initiation and Growth of 7050 Aluminum Alloy
Chaired by: M. ENRIGHT, Southwest Research Institute and R. TAYLOR, Optimal Structures, LLC 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1383 AIAA-2012-1384 AIAA-2012-1385 Study of Load Sequence Effects in Fatigue Reliability Analysis for High Random Fatigue Damage Combined Cyclic Fatigue Using CDM Cycle Fatigue Regime Accumulation under Variable N. Apetre, A. Arcari, S. Sarkar, N. Iyyer, Approach Amplitude Loading
K. Ni, Advanced Dynamics, Inc., Lexington, KY S. Sarkar, A. Arcari, N. Apetre, Technical Data Analysis, Inc., Falls Church, MD; N. Phan, P. Kang, Naval Air Systems Command, Patuxent River, VA
Fatigue and Fracture Mechanics I
Monday, 23 April 2012 9-SDM-5
Akaka Falls
Puna
Molokai
Kona
16
Martin Corporation, Fort Worth, TX
T. Field, A. Jones, M. Jansz, S. Raghavan, Gainesville, Gainesville, FL Y. Sohn, University of Central Florida, Orlando, FL; J. Okasinski, J. Almer, Argonne National Laboratory, Argonne, IL
J. Cotton, C. Frohlich, The Boeing Company, Seattle, WA
Nanostructured Materials I
A. Keskin, A. Saiz, Rolls-Royce Group plc, Derby, United Kingdom
1100 hrs AIAA-2012-1408 An Integrated Design System for Optimization of Gas Turbine Components
Madison, Madison, WI
P. van der Valk, D. Rixen, Delft University of Technology, Delft, The Netherlands
Chaired by: D. GRIFFITH and M. ALLEN, University of Wisconsin 1000 hrs 0930 hrs AIAA-2012-1415 AIAA-2012-1414 A Lifting Algorithm for Output-only Impulse Based Substructuring for Coupling Offshore Structures Continuous Scan Laser Doppler and Wind Turbines in Aero-Elastic Vibrometry S. Yang, M. Allen, University of Wisconsin, Simulations
Monday, 23 April 2012 16-SDM-12
Federal University of Minas Gerais, Belo Horizonte, Brazil; M. Triplett, Army Aviation and Missile Research Development and Engineering Center, Redstone Arsenal, AL
A. Achuthan, T. Arsenault, P. Marzocca, Clarkson University, Potsdam, NY; C. Grappasogni, G. Coppotelli, University of Rome “La Sapienza”, Rome, Italy
1030 hrs AIAA-2012-1416 Dynamic Identification of Wind Turbine System Under Operational Conditions Using FBG Transducers
M. Harte, Trinity College Dublin, Dublin, Ireland
1100 hrs AIAA-2012-1417 Soil-Foundation Models and Tower Transfer Functions for Offshore Wind Turbines
Wind Turbine Structural Dynamics
J. Koo, E. Allcorn, B. Johnson, M. Baek, S. Lao, University of Texas, Austin, Austin, TX; C. Lake, P. Lake, Applied Sciences, Inc., Cedarville, OH
Chaired by: S. ROY, University of Alabama; B. WARDLE, Massachusetts Institute of Technology and E. GLAESSGEN, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2012-1410 AIAA-2012-1411 AIAA-2012-1412 AIAA-2012-1413 Superhydrophobic Doped Synchrotron X-rays Monitoring Identification of Adhesive Bond in Multi-component Polyamide Nanomembranes: A New Approach Nano-Aluminum Grain Growth of Carbon Fiber Composites with a 11 Nanocomposites: Thermal, for Anti-Ice Formation on Wings a Metal Matrix Composite under ZnO Nanowire Interphase Mechanical, and Flammability A. Avila, J. de Avila, Jr., D. de Souza, G. Ehlert, H. Sodano, University of Florida, Properties Thermo-mechanical Conditions
Monday, 23 April 2012 15-SDM-11
Arlington, VA
J. Heeg, C. Wieseman, NASA Langley Research Center, Hampton, VA
1100 hrs AIAA-2012-1404 System identification and uncertainty quantification using orthogonal excitations and the Semispan Supersonic Transport (S4T) model
Air Vehicle Structural Dynamics I
W. LaCava, National Renewable Energy Laboratory, Golden, CO; B. McNiff, McNiff Light Industry, Dog Island, ME; Y. Guo, H. Link, National Renewable Energy Laboratory, Golden, CO
1130 hrs AIAA-2012-1418 NREL Gearbox Reliability Collaborative: Test and Model Investigation of Sun Orbit and Planet Load Share in a Wind Turbine Gearbox
J. Shi, T. Cook, J. Matlik, Rolls-Royce Group plc, Indianapolis, IN
1130 hrs AIAA-2012-1409 Integrated Computational Material Science and Engineering for Ceramic Matrix Composite Development
Integrated Computational Materials Engineering (ICME) I
J. Davis, Air Force Research Laboratory, Eglin AFB, FL; N. Kim, University of Florida, Gainesville, Gainesville, FL
1030 hrs AIAA-2012-1403 Control of the Flexural Axis of a SUAS Wing with Piezoelectric Actuation
Chaired by: J. MATLIK, Rolls-Royce Group plc and G. SEIDEL, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1405 AIAA-2012-1406 AIAA-2012-1407 ICME - A Revolution in Materials A Case Study on the Application of What Boeing Wants from Research Culture ICME in Aircraft Design Integrated Computational Materials J. Christodoulou, Office of Naval Research, D. Ball, T. Limer, R. Bridges, Lockheed Engineering for Metallic Materials
Monday, 23 April 2012 14-SDM-10
R. Palacios, Imperial College London, London, H. Hesse, J. Murua, R. Palacios, Imperial United Kingdom; M. Karpel, Technion--Israel College London, London, United Kingdom Institute of Technology, Haifa, Israel
Chaired by: D. RAVEH and S. SURAMPUDI, U.S. Air Force 0930 hrs 1000 hrs AIAA-2012-1401 AIAA-2012-1402 Intrinsic models for nonlinear flexible- Consistent Structural Linearization in Flexible Aircraft Dynamics with aircraft dynamics using industrial Large Rigid-Body Motion finite-element and loads packages
Monday, 23 April 2012 13-SDM-9
Kahuku
Waimea Canyon
Kohala
Waialua
17
T. Riddle, D. Cairns, J. Nelson, Montana State University, Bozeman, MT
J. Nelson, T. Riddle, D. Cairns, J. Workman, Montana State University, Bozeman, MT
K. Woo, Chungbuk National University, Cheongju, South Korea; M. Peterson, D. Cairns, J. Mandell, Montana State University, Bozeman, MT
Wright-Patterson AFB, OH
J. Zhang, Rensselaer Polytechnic Institute, D. Allaire, Q. He, K. Willcox, Troy, NY; A. Messac, Syracuse University, Massachusetts Institute of Technology, Syracuse, NY; J. Zhang, S. Chowdhury, Cambridge, MA Rensselaer Polytechnic Institute, Troy, NY
1700 hrs AIAA-2012-1428 Aircraft Design with Active Load Alleviation and Natural Laminar Flow
A. Dorobantu, University of Minnesota, S. Lacaze, S. Missoum, University of Minneapolis, Minneapolis, MN; L. Crespo, Arizona, Tucson, Tucson, AZ National Institute of Aerospace, Hampton, VA; P. Seiler, University of Minnesota, Minneapolis, Minneapolis, MN
1630 hrs AIAA-2012-1432 Fidelity maps for Model Update under Uncertainty: Application to a Piano Soundboard
T. Anderson, C. Mattson, Brigham Young University, Provo, UT
1700 hrs AIAA-2012-1433 Obtaining Non-Gaussian Output Error Distributions by Propagating Mean, Variance, Skewness, and Kurtosis Through Closed-Form Analytical Models
Design and Optimization Under Uncertainty
1630 hrs AIAA-2012-1427 An Investigation of Higher-order Multi-objective Optimisation for 3D Aerodynamic Shape Design
S. Liu, R. Canfield, Virginia Polytechnic Institute T. Kipouros, T. Ghisu, G. Parks, Cambridge J. Xu, I. Kroo, Stanford University, and State University, Blacksburg, VA University, Cambridge, United Kingdom; Stanford, CA A. Savill, Cranfield University, Cranfield, United Kingdom
1600 hrs AIAA-2012-1426 Continuum Shape Sensitivity Method for Fluid Flow Around an E. Alyanak, Air Force Research Laboratory, Airfoil
1530 hrs AIAA-2012-1425 Modeling for Conceptual Design: An Aeroelastic Approach
Chaired by: R. GRANDHI, Wright State University and F. VIANA, General Electric Company 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1429 AIAA-2012-1430 AIAA-2012-1431 Probability-based Sampling Using An Information-Theoretic Metric of Robustness Analysis and Optimally Distribution Fitting for Independent System Complexity with Application Robust Control Design via Sum-ofRandom Variables to Engineering System Design Squares
Monday, 23 April 2012 20-MDO-4
C. Guo, T. Kipouros, E. Shapiro, A. Savvaris, Cranfield University, Cranfield, United Kingdom
1500 hrs AIAA-2012-1424 On the Effects of Turbulence Modelling in Design Optimisation for High-lift Devices
D. Neufeld, Konkuk University, Seoul, South Korea
1730 hrs AIAA-2012-1434 A Multidisciplinary Possibilistic Approach to Light Aircraft Conceptual Design
1130 hrs AIAA-2012-1423 Fracture Analysis of Thick Adhesive Joints for Wind Turbine Blades
Tailoring of Composite Structures Using Spatially Varying Fiber Orientations Professor Michael Hyer N. Waldo Harrison Professor Emeritus of Engineering Science and Mechanics Virginia Polytechnic Institute and State University, Blacksburg, VA
SDM Lecture
P. Davidson, A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI; K. Chandraseker, W. Faidi, C. Yerramalli, General Electric Company, Niskayuna, NY
1100 hrs AIAA-2012-1422 Effect of Fiber Waviness on the Compressive Strength of Unidirectional Carbon Composites
Wind Turbine Composite Material Analysis
Monday, 23 April 2012 19-MDO-3 Aeroelastic and Aerodynamic Optimization Chaired by: R. CANFIELD, Virginia Polytechnic Institute and State University and E. PENDLETON, U.S. Air Force
Monday, 23 April 2012 18-SDM-14 1330 - 1430 hrs
Education, Monterrey, Mexico; P. Marzocca, Clarkson University, Potsdam, NY; F. Abdi, Alpha STAR Corporation, Long Beach, CA
Chaired by: F. ABDI, AlphaSTAR Corporation and D. CAIRNS, Montana State University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1419 AIAA-2012-1420 AIAA-2012-1421 Effects of Defects: Part B— Progressive Failure Analysis of Wind Effects of Defects: Part A— Progressive Damage Modeling Turbine Blades Based on a Thin-Wall Development of a Protocol for Defect Risk Management & of Fiberglass/Epoxy Composite Beam Finite Element Model D. Cardenas Fuentes, H. Elizalde, O. Probst, Improved Reliability of Composite Structures with Manufacturing Monterrey Institute of Technology and Higher Structures Induced Flaws
Monday, 23 April 2012 17-SDM-13
Hilo
Puna
Kauai
Waianae
18
Seoul, South Korea; C. Hu, University of Maryland, College Park, College Park, MD; T. Kim, Seoul National University, Seoul, South Korea; J. Chung, PCTEST Engineering Laboratory, Columbia, MD
T. Paez, MannaTech Engineering, Sandia Park, NM
Sierra Nevada Corporation, Louisville, CO
National Laboratories, Albuquerque, NM; T. Paez, Thomas Paez Consulting, Durango, CO
H. Shi, I. Fernandez Villegas, H. Bersee, Delft University of Technology, Delft, The Netherlands
Michigan, Ann Arbor, Ann Arbor, MI; B. Bednarcyk, S. Arnold, NASA Glenn Research Center, Cleveland, OH
1630 hrs AIAA-2012-1447 Fundamental Design of Tensioned Precision Deployable Space Structures Applied to an X-Band Phased Array
Design
B. Ravishankar, L. Wang, A. Subramaniyan, General Electric Company, Niskayuna, NY
1630 hrs AIAA-2012-1443 Probabilistic Validation Metrics for Industrial Engineering Analysis Models
M. Robinson, South Dakota School of Mines & Technology, Rapid City, SD; J. J. Kosmatka, E. Velazquez, University of California, San Diego, San Diego, CA; A. Pun, Kosmatka, University of California, San NextGen Aeronautics, Torrance, CA; J. Hunt, Diego, La Jolla, CA Naval Air Warfare Center, Patuxent River, MD
1630 hrs AIAA-2012-1451 Performance of Bonded/Bolted Hybrid Joints
Structural Joints
D. Bushnell, Self, Palo Alto, CA; C. Rankin, S. Jeon, Moog-CSA Engineering, Rhombus Consultants Group, Palo Alto, CA Albuquerque, NM; T. Murphey, Air Force Research Laboratory, Kirtland AFB, NM
Chaired by: S. SMELTZER, NASA Langely Research Center and S. ENGELSTAD, Lockheed Martin Corporation 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1449 AIAA-2012-1450 AIAA-2012-1448 Co-rotational Formulation for Simplified Methods for Automated An investigation on the strain Bonded Joint Finite Elements Modeling of Riveted/Bolted distribution of resistance welded S. Stapleton, A. Waas, University of Connections in Flight Structures thermoplastic composite joints
Monday, 23 April 2012 24-SDM-16
Materials, Inc., Hampton, VA
Chaired by: E. LUNDGREN, The Aerospace Corporation and M. DOMB, Bombardier, Inc. 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1444 AIAA-2012-1445 AIAA-2012-1446 Repair Concepts as Design Design, Analysis, and Test of the Use of GENOPT and BIGBOSOR4 Constraints of a Stiffened QwkSep Sub 24-inch Low-Profile to Obtain Optimum Designs of Composite PRSEUS Panel Separation System Multiwalled Inflatable Spherical A. Przekop, Analytical Services and V. Stavast, C. Lazansky, B. Helgesen, and Cylindrical Vacuum Chambers
Monday, 23 April 2012 23-SDM-15
L. Campo, D. Helmer, J. Eaton, Stanford University, Stanford, CA
S. Leem, D. An, J. Choi, Korea Aerospace University, Goyang, South Korea
1700 hrs AIAA-2012-1439 On-Experimental Validation of Crack Growth Prognosis under Variable Amplitude Loads
F. Bianchi, X. Zhang, Cranfield University, Bedford, United Kingdom
1700 hrs AIAA-2012-1452 A numerical model for hybrid metal-composite joints with through-thickness reinforcement
Uncertainty Quantification in Verification and Validation II
D. Cope, Southwest Research Institute, K. Halbert, L. Fitzwater, C. Davis, J. Ihn, D. San Antonio, TX Jones, J. Mcfarland, T. Torng, D. Wiegand, The Boeing Company, Chicago, IL
Chaired by: G. IACCARINO, Stanford University and B. THACKER, Southwest Research Institue 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1440 AIAA-2012-1441 AIAA-2012-1442 Validation Experiment for Shock Validation of Using Linear Models The Verification and Uncertainty Boundary Layer Interactions: for Nonlinear Structures Quantification of Surrogate Models Sensitivity to Upstream Geometric M. Ross, A. Urbina, N. Hunter, Sandia Used for Structural Analysis National Laboratories, Albuquerque, NM; M. Ross, A. Urbina, T. Simmermacher, Sandia Perturbations
Monday, 23 April 2012 22-NDA-4
Goyang, South Korea; N. Kim, University of Florida, Gainesville, Gainesville, FL
1630 hrs AIAA-2012-1438 Bayesian Updating of Structural Health and Integrity Assessments using Real-Time Inspection Results
Non-Deterministic Approaches to Structural Health Management II
Chaired by: J. RANSOM, NASA Langley Research Center and N. KIM, University of Florida 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1435 AIAA-2012-1436 AIAA-2012-1437 Online State-of-Health Prediction Cost/Benefit Analysis for A Comparison Study of Methods of Lithium-Ion Battery with a System-Level Integration of for Parameter Estimation in the Multiscale Filtering Technique Non-Deterministic Analysis and Physics-based Prognostics D. An, J. Choi, Korea Aerospace University, B. Youn, Seoul National University, Maintenance Technology
Monday, 23 April 2012 21-NDA-3
X. Zhang, Y. Liu, J. Ren, Beihang University, Beijing, China; K. Zhan, George Washington University, Washington, DC, WA
1730 hrs AIAA-2012-1453 Nonlinear Finite Element Analysis of the SRM Flexible Joint
Waianae
Oahu
Kauai
Honolulu
19
A. Rhead, R. Butler, University of Bath, Bath, United Kingdom
L. Demasi, R. Cavallaro, San Diego State University, San Diego, CA
C. Merrett, Carleton University, Ottawa, Canada; H. Hilton, University of Illinois, Urbana-Champaign, Urbana, IL
1600 hrs AIAA-2012-1456 The Influence of Unsymmetrical Bending and Torsion on Elastic and Viscoelastic Wing Flutter
A. Kayran, E. Yavuzbalkan, S. Ibrahimoglu, Middle East Technical University, Ankara, Turkey
G. Vio, University of Sydney, Sydney, R. Moreno, P. Taylor, Gulfstream Aerospace Australia; G. Dimitriadis, University of Corporation, Savannah, GA; J. Newsom, Liège, Liège, Belgium Newsom Aerospace Consulting, LLC, Poquoson, VA
1600 hrs AIAA-2012-1466 Computational Identification of Non-Linear Damping in an Aeroelastic System
University London, London, United Kingdom
Chaired by: I. CHOPRA, University of Maryland and P. PAI, University of Missouri 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1471 AIAA-2012-1472 AIAA-2012-1470 Characterizing Plate Damping Loss Investigation of the Effect of Geodesic Dynamic Stiffness Formulation and and Semi-geodesic Winding on the Free Vibration Analysis of Composite Factor Estimation Errors Plate Assemblies using Higher Order M. Ewing, H. Dande, University of Kansas, Vibration Characteristics of Variable Lawrence, Lawrence, KS Stiffness Filament Wound Shells of Shear Deformation Theory F. Fazzolari, M. Boscolo, J. Banerjee, City Revolution
Monday, 23 April 2012 28-SDM-20
Scott, NextGen Aeronautics, Torrance, CA
Chaired by: J. COOPER, University of Bristol 1500 hrs 1530 hrs AIAA-2012-1464 AIAA-2012-1465 Wind Tunnel Test of a Very Flexible A Rigid Horizontal Tail Wind Tunnel Aircraft Wing Test for High Transonic Mach and R. Britt, D. Ortega, J. Mc Tigue, The High Frequency Unsteady Pressure Boeing Company, Seal Beach, CA; M. Acquisition
Monday, 23 April 2012 27-SDM-19
W. Liu, R. Butler, H. Kim, University of Bath, Bath, United Kingdom
Chaired by: L. HARDAWAY, Ball Aerospace & Technologies Corporation and T. LACY, Mississippi State University 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1460 AIAA-2012-1461 AIAA-2012-1462 Buckling Optimization of Variable Compressive Strength Following Nonlinear Analysis of PrandtlPlane Angle Tow Panels Using Exact Strip Delamination Induced Interaction Joined Wings. Part II: Effects of Models of Panel and Sublaminate Buckling Anisotropy
Monday, 23 April 2012 26-SDM-18
Polytechnic Institute and State University, M. Snyder, T. Weisshaar, Purdue Blacksburg, VA; N. Lindsley, Air Force Research University, West Lafayette, IN Laboratory, Wright-Patterson AFB, OH
Chaired by: H. HILTON and P. RANATUNGA, Miami Univeristy 1500 hrs 1530 hrs AIAA-2012-1454 AIAA-2012-1455 Nonlinear Aeroelastic Scaling of a Flutter and Directional Stability of Aircraft with Wing Tip-Fins - Conflict Joined Wing Aircraft A. Ricciardi, R. Canfield, M. Patil, Virginia and Compromises
Monday, 23 April 2012 25-SDM-17
M. Boscolo, J. Banerjee, City University London, London, United Kingdom
1630 hrs AIAA-2012-1473 Dynamic Stiffness Laminate Elements for Exact Modal Analysis of Aeronautical Structures
Plate and Shell Dynamics
Y. Dai, C. Yang, Z. Wu, L. Chen, Beihang University, Beijing, China
1630 hrs AIAA-2012-1467 Aeroelastic Wind Tunnel Test for Aerodynamic Uncertainty Model Validation
Aeroelastic Testing
Z. Wu, G. Raju, P. Weaver, University of Bristol, Bristol, United Kingdom
I. Fitspatrick, G. Vio, University of Sydney, Sydney, Australia; J. Cooper, G. Georgiou, University of Liverpool, Liverpool, United Kingdom
1700 hrs AIAA-2012-1458 Design of Composite Structures to Improve the Aeroelastic Performance
Y. Na, S. Shin, Seoul National University, Seoul, South Korea
1700 hrs AIAA-2012-1474 Equivalent Plate Analysis of a Composite Wing with a Control Surface
1730 hrs AIAA-2012-1469 Design and Analysis of a Wind Tunnel Test Model System for Gust Alleviation of Aeroelastic Aircraft
C. Xie, Y. Liiu, C. Yang, Beihang University, Beijing, China
1730 hrs AIAA-2012-1459 Static Aeroelastic Analysis of Very Flexible Wing Based on the 3-D Lifting-Line Theory
G. Wang, University of Alabama, Huntsville, Huntsville, AL
1730 hrs AIAA-2012-1475 Free Vibration of Stepped Thickness Rectangular Plates Using Spectral Finite Element Method
Z. Wu, Beihang University, Beijing, China; L. Wang, L. Shen, L. Chen, Z. Wu, C. Z. Jing, Xi’an Institute of Aircraft Design Yang, Beihang University, Beijing, China and Research, Xi’an, China; C. Yang, Beihang University, Beijing, China
1700 hrs AIAA-2012-1468 Dynamic Response Analysis and Experimental Validation for Airdrop of a Flexible Aircraft
1630 hrs AIAA-2012-1463 Buckling of VAT Plates Using Energy Methods
Buckling of Composites
C. York, University of Glasgow, Glasgow, United Kingdom
1630 hrs AIAA-2012-1457 Extension-Twisting coupled laminates for aero-elastic compliant blade design
Aeroelasticity and Flutter
Koko Crater
Molokai
Waialua
Lanai
20
University of Michigan, Ann Arbor, Ann Arbor, MI
C. Langston, Army Research Laboratory, Hampton, VA
H. Jou, A. Misra, C. Kuehmann, QuesTek Innovations, LLC, Evanston, IL
University, College Station, TX
Champaign, Urbana, IL
Columbia, Columbia, SC
W. McLendon, J. Whitcomb, Texas A&M University, College Station, TX
1700 hrs AIAA-2012-1497 Aeroelastic Simulation of Structures in Hypersonic Flow R. Brown, K. Das, P. Cizmas, J. Whitcomb, X. Ren, G. Seidel, Virginia Polytechnic Institute Texas A&M University, College Station, TX and State University, Blacksburg, VA
1630 hrs AIAA-2012-1496 Analytic and Computational Multi-scale Micromechanics Piezoresistive Models for Fuzzy Fiber Composite Material
D. Betts, H. Kim, C. Bowen, University of Bath, Bath, United Kingdom; D. Inman, University of Michigan, Ann Arbor, Ann Arbor, MI
S. Sinha, General Electric Company, Cincinnati, OH; S. Ojha, General Electric Company, Bangalore, India
1730 hrs AIAA-2012-1481 Rotordynamic Analysis of Asymmetric Turbofan Rotor Due to Fan Blade-out Event with ContactImpact Rub Loads
1730 hrs AIAA-2012-1492 Static and Dynamic Analysis of Bistable Piezoelectric-Composite V. Giurgiutiu, University of South Carolina, Plates for Energy Harvesting
1700 hrs AIAA-2012-1491 Predictive Simulation of Structural Sensing
Hybrid Materials for Hypersonic Vehicles (MURI)
IN; H. Sehitoglu, University of Illinois, Urbana- T. Rodgers, H. Zhao, H. Wadley, University of Champaign, Urbana, IL; H. Maier, University Virginia, Charlottesville, Charlottesville, VA of Paderborn, Paderborn, Germany; D. Furrer, M. Glavicic, J. Stillinger, Rolls-Royce Group plc, Indianapolis, IN
1630 hrs AIAA-2012-1490 Integrated Development of Vapor Deposition for Non-line-of-sight M. Sangid, Purdue University, West Lafayette, Substrates
Chaired by: G. SEIDEL, Virginia Polytechnic Institute and State University and D. LAGOUDAS, Texas A&M University 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1494 AIAA-2012-1495 AIAA-2012-1493 Computational Design of Actively- Failure Initiation Prediction in Computational Micromechanical Cooled Microvascular Composites Textile Composites Under Complex Modeling of Ceramic-SMA for High Temperature Applications Thermo-Mechanical Loading Based Composites B. Lester, D. Lagoudas, Texas A&M P. Geubelle, University of Illinois, Urbana- on Meso-scale Analysis
Monday, 23 April 2012 32-SDM-24
S. Christensen, The Boeing Company, Seattle, WA
1700 hrs AIAA-2012-1486 Rate-free Control of Nonlinear Wing Section Using Pitch and Plunge Measurements Only
F. Ulker, F. Nitzsche, Carleton University, Ottawa, Canada
1700 hrs AIAA-2012-1480 Advances in Helicopter Vibration Control Methods
Integrated Computational Materials Engineering (ICME) II
1630 hrs AIAA-2012-1485 Receptance Based Active Aeroelastic Control Using Multiple Control Surfaces
Controls
Y. Chen, V. Wickramasinghe, D. Zimcik, National Research Council Canada, Ottawa, Canada
1630 hrs AIAA-2012-1479 Identification of Aeroelastic Parameters for Cormorant Tail Rotor Structures based on Vibration Measurement in the Stationary Frame
RotorCraft Dynamics
J. Murua, R. Palacios, J. Graham, Imperial K. Singh, L. McDonough, Miami University, N. Satak, E. Peraza Hernandez, J. College, London, United Kingdom Oxford, OH; R. Kolonay, Air Force Research Hurtado, Texas A&M University, College Laboratory, Wright-Patterson AFB, OH; J. Station, TX Cooper, University of Liverpool, Liverpool, United Kingdom
1600 hrs AIAA-2012-1484 Open-Loop Stability and ClosedLoop Gust Alleviation on Flexible Aircraft Including Wake Modeling
Chaired by: J. MATLIK, Rolls-Royce Group plc and S. ROY, University of Alabama 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1488 AIAA-2012-1489 AIAA-2012-1487 Precipitation Modeling for Role of Microstructure in Predicting Computational Methods for New Materials Development Accelerated Alloy Development Fatigue Performance
Monday, 23 April 2012 31-SDM-23
B. Glaz, Army Research Laboratory, Aberdeen B. Alstrom, Clarkson University, Potsdam, NY Proving Ground, MD; M. McCrink, D. Gaitonde, Ohio State University, Columbus, OH; S. Dinavahi, Lockheed Martin Corporation, Aberdeen Proving Ground, MD
Chaired by: L. ROBERTSON, Air Force Reseach Laboratory 1500 hrs 1530 hrs AIAA-2012-1482 AIAA-2012-1483 Nanosecond Pulsed Plasma Actuation The Application of Nonlinear PreEffects on Aerodynamic Damping and Filters to Prevent Aeroservoelastic Aeroelastic Stability Implications in the Interactions Due to Actuator Rate Post-Stall Regime Limiting
Monday, 23 April 2012 30-SDM-22
A. Overmeyer, J. Palacios, E. Smith, Pennsylvania State University, University Park, PA
Chaired by: D. JOHNSON, NASA Glenn Research Center and D. PITT, The Boeing Company 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1476 AIAA-2012-1477 AIAA-2012-1478 Actuator Bonding Optimization and Actuator Saturation in Individual Experimental Bench Testing of an Blade Control of Rotorcraft Active-Twist Rotor Blade System Control of a Rotor Blade P. Friedmann, A. Padthe, D. Bernstein, A. Kreshock, R. Thornburgh, M. Wilbur, Ultrasonic Deicing System
Monday, 23 April 2012 29-SDM-21
Niihau
Kohala
Waimea Canyon
Akaka Falls
21
A. Pirrera, N. Buckney, P. Weaver, University of Bristol, Bristol, United Kingdom
1600 hrs AIAA-2012-1500 Optimization of Wind Turbine Blade Spars
Chaired by: V. BALABANOV, The Boeing Company
Tuesday, 24 April 2012 36-MDO-5 0800 - 0900 hrs
Monday, 23 April 2012 35-RCTP-1 1800 - 1930 hrs
Tuesday
Reception
J. Williamsen, Institute for Defense Analyses, Alexandria, VA; W. Schonberg, Missouri University of Science and Technology, Rolla, MO
M. Shimek, E. Fahrenthold, University of Texas, Austin, Austin, TX
Natalia Alexandrov Senior Research Scientist NASA Langley Research Center
M. McWilliam, C. Crawford, University of Victoria, Victoria, Canada
1730 hrs AIAA-2012-1503 Adjoint Based Sensitivity Analysis for Geometrically Exact Beam Theory and Variational Asymptotic Beam Section Analysis with Applications to Wind Turbine Design Optimization
1700 hrs AIAA-2012-1508 Effects of Weave Type on Ballistic Performance for Aramid, UHMWPE, and Hybrid Fabrics
N. Buckney, S. Green, A. Pirrera, P. Weaver, University of Bristol, Bristol, United Kingdom
1700 hrs AIAA-2012-1502 Wind Turbine Blade Structural Efficiency
Multidisciplinary Design Optimization: What Remains to be Done
M. Buck, J. Murphy, J. Bestard, B. Kocher, S. Sinha, General Electric Company, Cincinnati, AFB, OH; G. Rogers, U.S. Air Force, Hill AFB, UT U.S. Air Force, Wright-Patterson AFB, OH OH; G. Czarnecki, U.S. Air Force, WrightPatterson AFB, OH; R. Hinrichsen, RHAMM Technologies, Bellbrook, OH
1630 hrs AIAA-2012-1507 An Improved Prediction Model for Spacecraft Damage Following Orbital Debris Impact
Air and Space Survivability
M. Capellaro, University of Stuttgart, Stuttgart, Germany
1630 hrs AIAA-2012-1501 Design Limits of Bend Twist Coupled Wind Turbine Blades
Wind Turbine Blade Design, Analysis, and Optimization
Chaired by: E. FAHRENTHOLD, University of Texas and J. KLOOS, General Electric Company 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1504 AIAA-2012-1505 AIAA-2012-1506 Hydrodynamic Ram Model Dynamic Analysis of Damage to Assessing Survivability Increasing Development - Survivability the Aircraft Propulsion System Technologies in the A-10 Aircraft Analysis Requirements Impacted by an Exploding Missile J. Kemp, U.S. Air Force, Wright-Patterson
Monday, 23 April 2012 34-SDM-26
T. Kim, C. Bak, Risø Technical University of T. Ashwill, B. Resor, D. Griffith, Sandia Denmark, Roskilde, Denmark National Laboratories, Albuquerque, NM
Chaired by: B. RESOR, Sandia National Laboratories and W. YU 1500 hrs 1530 hrs AIAA-2012-1498 AIAA-2012-1499 Large Offshore Rotor Development: Parametric Studies of Composite Blade to Improve the Wind Turbine Design and Analysis of the Sandia 100-meter Wind Turbine Blade Response
Monday, 23 April 2012 33-SDM-25
Kauai
Poolside
Kona
Kahuku
22
University, Swansea, United Kingdom
D. Lichodziejewski, C. Kelley, B. Tutt, Airborne Systems, Santa Ana, CA; G. Brown, D. Jurewicz, HDT, Lake Elsinore, CA; D. Barber, Oceaneering, Houston, TX; R. Dillman, C. Player, NASA Langley Research Center, Hampton, VA
1100 hrs AIAA-2012-1512 Piezoelectric Morphing versus ServoActuated MAV Control Surfaces
Aerospace System Applications I
M. Erford, E. Henry, J. Nay, J. Slater, Wright State University, Dayton, OH
1030 hrs AIAA-2012-1516 Flight Dynamics System Identification of a Free Falling Ballute
G. Kennedy, University of Toronto, Toronto, Everett, WA; O. Weckner, M. Epton, G. S. Salehghaffari, M. Rais-Rohani, D. Liu, V. Toropov, University of Leeds, Canada; J. Martins, University of Michigan, Mabson, S. Cregger, A. Blom, The Boeing Mississippi State University, Starkville, MS Leeds, United Kingdom Company, Seattle, WA Ann Arbor, Ann Arbor, MI
1100 hrs AIAA-2012-1522 Ply number rounding-off in optimization of composite structures using lamination parameters
Optimization of Composites
T. Sinn, M. Vasile, University of Strathclyde, Glasgow, United Kingdom; G. Tibert, Royal Institute of Technology (KTH), Stockholm, Sweden
1100 hrs AIAA-2012-1517 Design and Development of a Deployable Self-inflating Adaptive Membrane
Inflatable Structures
O. Ohanian, E. Karni, C. Olien, B. Stiltner, Barnhart, University of Kansas, Lawrence, C. Hickling, AVID, LLC, Blacksburg, VA; K. Lawrence, KS Kochersberger, T. Probst, Virginia Polytechnic Institute and State University, Blacksburg, VA; P. Gelhausen, AVID, LLC, Yorktown, VA; A. Blain, Air Force Research Laboratory, Eglin AFB, FL
Chaired by: V. LI, The Boeing Company and O. WECKNER, The Boeing Company 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1520 AIAA-2012-1521 AIAA-2012-1519 A Regularized Discrete Laminate Optimal Design of a Composite Evidence-Based Design Parametrization Technique with Sandwich Structure Using Optimization of Energy Absorbing Applications to Wing-Box Design Lamination Parameters Components under Material Field V. Balabanov, The Boeing Company, Optimization Uncertainty
Tuesday, 24 April 2012 39-MDO-6
J. Hinkle, J. Lin, ILC Dover, Frederica, DE
Chaired by: C. WILLEY, ILC Dover and G. LAUE, SRS Technologies 0930 hrs 1000 hrs AIAA-2012-1514 AIAA-2012-1515 Design and Testing of an Design and Testing of the Inflatable Expandable Space Structure Using Aeroshell for the IRVE-3 Flight Softgoods Composite Technology Experiment
Tuesday, 24 April 2012 38-GSF-1
D. Kim, Embry-Riddle Aeronautical University, Daytona Beach, FL; M. Philen, R. Capps, S. Hutchinson, Virginia Polytechnic Institute and State University, Blacksburg, VA
Chaired by: G. REICH, Air Force Reseach Laboratory and D. MCGOWAN, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1509 AIAA-2012-1510 AIAA-2012-1511 Span Morphing: A Conceptual Steerable Adaptive Bullet Flight Morphing Trailing Edge Control Design Study Control Mechanism Design Using Flexible Matrix Composite O. Little, R. Ajaj, M. Friswell, Swansea R. Barrett-Gonzalez, R. Bramlette, R. Actuators
Tuesday, 24 April 2012 37-ASC-1
R. Robinson, University of Maryland, College Park, College Park, MD; C. Kothera, Techno-Sciences, Inc., Beltsville, MD; N. Wereley, University of Maryland, College Park, College Park, MD
1130 hrs AIAA-2012-1518 Control of a Heavy-Lift Robotic Manipulator with Pneumatic Artificial Muscles
J. Xie, Z. Yang, Northwestern Polytechnical University, Xi’an, China; S. Guo, Cranfield University, Milton Keynes, United Kingdom
1130 hrs AIAA-2012-1513 Aerodynamic and Aeroelastic Characteristics of Conformal Control Surfaces and Application in Active Aeroelastic Wing Technology
Puna
Honolulu
Lanai
23
J. Holub, J. Foo, V. Kalivarapu, E. Winer, Iowa State University, Ames, IA
F. Laun, B. Taft, Air Force Research Laboratory, Kirtland AFB, NM
J. Allison, University of Illinois, UrbanaChampaign, Urbana, IL
1100 hrs AIAA-2012-1526 Engineering System Co-Design with Limited Plant Redesign
Optimization Applications II
J. Zhang, S. Chowdhury, Rensselaer Polytechnic Institute, Troy, NY; A. Messac, Syracuse University, Syracuse, NY
1130 hrs AIAA-2012-1527 Surrogate-Based Optimization Using Adaptive Hybrid Functions
H. Lin, G. Subbarayan, Purdue University, West Lafayette, IN
1100 hrs AIAA-2012-1531 Quantification of Behavioral Uncertainty Resulting from Insertion of Heterogeneity into Microstructure
NM; T. Murphey, B. Taft, Air Force Research Research Laboratory, Kirtland AFB, NM Laboratory, Kirtland AFB, NM; S. Pedrotty, New Mexico State University, Las Cruces, NM
D. Hengeveld, LoadPath, Albuquerque, NM; D. Doyle, W. Reynolds, Air Force Research Laboratory, Kirtland AFB, NM; K. Taft, New Mexico State University, Las Cruces, NM
1100 hrs AIAA-2012-1535 Ultrasonic Characterization as a Correlating Metric for Evaluating Thermal Contact Resistance
Structural and Thermal Interactions of Aerospace Systems
Vienna, VA; J. Stillinger, Rolls-Royce Group R. Ghanem, A. Noshadravan, University plc, Indianapolis, IN; D. Buede, J. Tatman, of Southern California, Los Angeles, Los Innovative Decisions, Inc., Vienna, VA Angeles, CA
1030 hrs AIAA-2012-1530 Identfication and validation of a stochastic model for mesoscale material description of metallic polycrystals
Integrated Computational Materials Engineering (ICME) III
Chaired by: J. DIDION, NASA Goddard Space Flight Center and A. WILLIAMS, Air Force Research Laboratory 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1533 AIAA-2012-1534 AIAA-2012-1532 Structural Integration of Pulsating Thermal Characterization of Structural Performance of a GridHeat Pipes in Printed Circuit Boards Graphite Storable Tubular Stiffened Panel with Integrated and Facesheets of Honeycomb Extendable Masts Thermal Control D. Hengeveld, LoadPath, Albuquerque, G. Busch, N. Doane, A. Williams, Air Force Panels
Tuesday, 24 April 2012 42-SDM-27
R. McClung, M. Enright, W. Liang, J. Moody, Southwest Research Institute, San Antonio, TX; W. Wu, R. Shankar, W. Luo, J. Oh, Scientific Forming Technologies Corporation, Columbus, OH; S. Fitch, Elder Research, Charlottesville, VA
Chaired by: J. MATLIK, Rolls-Royce Group plc 0930 hrs 1000 hrs AIAA-2012-1528 AIAA-2012-1529 Integration of Manufacturing Process Towards a Probabilistic Framework Simulation with Probabilistic Damage for Integrated Computational Tolerance Analysis of Aircraft Engine Materials Engineering S. Mahoney, Innovative Decisions, Inc., Components
Tuesday, 24 April 2012 41-NDA-5
A. Fraj, M. Budinger, T. El Halabi, INSA Toulouse, Toulouse, France; G. Negoita, Polytechnic University of Bucharest, Bucharest, Romania; J. Mare, INSA Toulouse, Toulouse, France
Chaired by: N. CHENNIMALAI KUMAR and M. NIKBAY, Istanbul Technical University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1523 AIAA-2012-1524 AIAA-2012-1525 Aircraft Route Optimization for Three Dimensional Multi-Objective Modelling approaches for the UAV Path Planning Using Digital simulation-based preliminary design Heterogeneous Formation Flight and optimization of electromechanical J. Xu, S. Ning, G. Bower, I. Kroo, Stanford Pheromone Particle Swarm University, Stanford, CA and hydraulic actuation systems Optimization
Tuesday, 24 April 2012 40-MDO-7
Kona
Kauai
Hilo
24
Michigan, Ann Arbor, Ann Arbor, MI
Nashville, TN
W. Ji, A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI; R. Raveendra, Comet Technology Corporation, Ann Arbor, MI
Columbus, OH; H. Johnson, University of Minnesota, Minneapolis, Minneapolis, MN
Laboratory, Wright-Patterson AFB, OH
C. Chamis, NASA Glenn Research Center, Cleveland, OH
B. Miller, J. McNamara, Ohio State University, Columbus, OH
Chaired by: J. MCNAMARA, Ohio State University and S. COLE, NASA Langley Research Center 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1549 AIAA-2012-1550 AIAA-2012-1548 Hypersonic Boundary Layer Application of Reduced-Order Modeling and Analysis of Shock Stability in the Presence of Thermo- Models for Thermoelastic Trajectory Impingements on ThermoMechanical Surface Compliance Simulation Mechanically Compliant Surface Z. Riley, J. McNamara, Ohio State University, J. Hollkamp, R. Gordon, Air Force Research Panels
Tuesday, 24 April 2012 46-SDM-31
Lockheed Martin Corporation, Fort Worth, TX
I. Guven, K. Colavito, E. Madenci, University of Arizona, Tucson, Tucson, AZ
1100 hrs AIAA-2012-1542 Fracture Behavior of Nanostructured Materials through Peridynamic Theory
Fatigue and Fracture Mechanics II
G. Li, Z. Wan, Beihang University, Beijing, China
1100 hrs AIAA-2012-1551 Aerothermal-Aeroelastic Two-way Coupling Method for Hypersonic Flutter of Three-Dimensional Curved Panel
Aerothermal Dynamics
B. Bednarcyk, NASA Glenn Research Center, Cleveland, OH; P. Yarrington, Collier Research Corporation, Newport News, VA; S. Arnold, NASA Glenn Research Center, Cleveland, OH
1100 hrs AIAA-2012-1546 Multiscale Fatigue Life Prediction for Composite Panels
M. Michaeli, A. Shtark, H. Grosbein, Israel Military Industries, Ramat Gan, Israel; H. Hilton, University of Illinois, UrbanaChampaign, Urbana, IL
1130 hrs AIAA-2012-1547 Characterization of Isotropic Viscoelastic Moduli and Compliances from 1-D Tension Experiments
Special Session II in Honor of Professor Michael W. Hyer
Chaired by: T. OCHINERO, Structural Mechanics Corporation and M. SCHULTZ, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1543 AIAA-2012-1544 AIAA-2012-1545 Industry Perspectives on Composite Progressive Failure Analysis Multi-scale Multi-functional Structural Certification and Design Method of a Pi Joint with Progressive Fracture of Composite C. Rousseau, S. Engelstad, S. Owens, Uncertainties in Fracture Properties Structures
Tuesday, 24 April 2012 45-SDM-30
J. Zhang, C. Luo, A. Chattopadhyay, Arizona State University, Tempe, AZ
Chaired by: S. WANTHAL, The Boeing Company and S. KUMARI, Pratt & Whitney 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1538 AIAA-2012-1540 AIAA-2012-1541 A Statistical Volume Element Based Peridynamics Based on the Uncertainty Quantification In NonApproach to Multiscale Modeling Principle of Virtual Work planar Crack Growth Analysis V. Hombal, K. Wolfe, Y. Ling, S. of Fatigue Crack Formation in AA E. Oterkus, E. Madenci, A. Barut, University of Arizona, Tucson, Tucson, AZ Mahadevan, Vanderbilt University, 2024-T351
Tuesday, 24 April 2012 44-SDM-29
1100hrs AIAA-2012-1615 Multiscale Modeling of Damage Accumulation in Carbon Fiber Reinforced Polymers Subjected to Fatigue
Fatigue and Fracture of Composites
R. Crouch, C. Oskay, Vanderbilt University, Nashville, TN; S. Clay, Air Force Research E. Pineda, A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI; B. Bednarcyk, NASA Laboratory, Wright-Patterson AFB, OH Glenn Research Center, Cleveland, OH
Chaired by: M. CHO, Seoul National University and P. GUSTAFSON, Western Michigan University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1536 AIAA-2012-1537 AIAA-2012-1539 Investigation of progressive Progressive Failure of a On the mesh dependency of damage and fracture in laminated Unidirectional Fiber-reinforced cohesive zone models for crack composites using the smeared Composite Using the Method of propagation analysis J. Rimoli, J. Rojas, F. Khemani, Georgia crack approach Cells: Discretization Objective Institute of Technology, Atlanta, GA C. Heinrich, A. Waas, University of Computational Results
Tuesday, 24 April 2012 43-SDM-28
Akaka Falls
Oahu
Waialua
Waianae
25
Maryland, College Park, College Park, MD Y. Wang, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Inman, University of Michigan, Ann Arbor, Ann Arbor, MI
Air Vehicle Structural Dynamics II
1130 hrs AIAA-2012-1988 Discrete Vortex Simulations of the torsional flutter oscillations of a 4:1 rectangular cylinder
T. Andrianne, G. Dimitriadis, University of Liverpool, United Kingdom; M. Wu, University Z. Wang, Z. Zhang, P. Chen, D. Sarhaddi, Liège, Liège, Belgium of Maryland, College Park, MD; A. Spence, ZONA Technology, Inc., Scottsdale, AZ; W. University of Bath, Bath, United Kingdom Yu, Utah State University, Logan, UT
1100 hrs AIAA-2012-1564 Enabling Sensitivity Analysis Capability for a CFD-Based Unsteady Aerodynamic/Aeroelastic Solver
Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and G. GURUSWAMY, NASA Ames Research Center 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1562 AIAA-2012-1563 AIAA-2012-1561 Towards CFD Based Aeroservoelastic Coupled CSD/CFD non-linear Lyapunov Inverse Iteration Flight Vehicle Shape Optimization aeroelastic trim of free-flying for Stability Analysis using New Capabilities and New Results with flexible aircraft Computational Fluid Dynamics G. Romanelli, M. Castellani, S. Ricci, S. Timme, K. Badcock, University of Liverpool, ZEUS-DO
Z. Zhang, P. Chen, ZONA Technology, Inc., Technical University of Milan, Milan, Italy Scottsdale, AZ; E. Livne, University of Washington, Seattle, Seattle, WA
Computational Aeroelasticity I
Tuesday, 24 April 2012 49-SDM-34
Liverpool, Liverpool, United Kingdom
1130 hrs AIAA-2012-1556 Computational Aeroelastic Analysis of the Semi-Span Super-Sonic Transport (S4T) Wind-Tunnel Model
D. Christhilf, Lockheed Martin Corporation, M. Sanetrik, W. Silva, NASA Langley Research Center, Hampton, VA; J. Hur, J. Florance, R. Scott, D. Keller, M. C. Wieseman, NASA Langley Research Center, Hampton, VA; K. Roughen, M4 Lockheed Martin Corporation, Hampton, VA Sanetrik, W. Silva, B. Perry, NASA Langley Hampton, VA; D. Christhilf, Lockheed Martin Engineering, Inc., Long Beach, CA; B. Moulin, E. Ritz, P. Chen, ZONA Technology, Research Center, Hampton, VA Corporation, Hampton, VA Inc., Scottsdale, AZ; B. Perry, NASA Langley Research Center, Hampton, VA
1100 hrs AIAA-2012-1555 Characteristics of Control Laws Tested on the Semi-Span Super-Sonic Transport (S4T) Wind-Tunnel Model
Semi-Span Supersonic Transport
Chaired by: F. UDWADIA, University of Southern Californa and V. WICKRAMASINGHE 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1557 AIAA-2012-1559 AIAA-2012-1560 Rapid Prediction of Worst Case Active Control of Performance and Experimental Validation of a Gust Loads Following Structural Vibratory Loads Using Leading Multifunctional Wing Spar Design Modification Edge Slats with Sensing, Harvesting and Gust H. Khodaparast, J. Cooper, University of I. Chopra, K. Ravichandran, University of Alleviation Capabilities
Tuesday, 24 April 2012 48-SDM-33
C. Wieseman, W. Stevens, C. Funk, J. Hur, D. Christhilf, Lockheed Martin Corporation, Hampton, VA; D. Coulson, Analytical Services and Materials, Hampton, VA
Chaired by: R. SCOTT, NASA Langley Research Center and B. PERRY, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1552 AIAA-2012-1553 AIAA-2012-1554 Lessons in the Design and Analytical and Experimental An Overview of the Semi-Span Evaluation of Digital Control Super-Sonic Transport (S4T) Wind- Characterization Testing of the Semi-Span Super-Sonic Transport Systems for the Semi-Span SuperTunnel Model Program W. Silva, B. Perry, J. Florance, M. Sanetrik, (S4T) Wind-Tunnel Model Sonic Transport (S4T) Project
Tuesday, 24 April 2012 47-SDM-32
Koko Crater
Niihau
Molokai
26
1030 hrs AIAA-2012-1567 Effect of Manufacturing Route on Mode I Fracture Toughness of Aligned Carbon Nanotube Reinforced Composites
France; C. Tonon, M. Chevalier, C. Puig, EADS, Toulouse, France; H. Combes, P. Guigue, C. Durin, French Space Agency (CNES), Toulouse, France; C. Lacabanne, National Center for Scientific Research (CNRS), Toulouse, France
J. Mandell, D. Samborsky, D. Miller, Montana State University, Bozeman, MT
Chaired by: J. MANDELL 0930 hrs AIAA-2012-1573 The SNL/MSU/DOE Fatigue of Composite Materials Database: Recent Trends
Tuesday, 24 April 2012 52-SDM-37
1100 hrs AIAA-2012-1571 Experimental Investigation of Anisotropy in Mechanical Response of Acrylonitrile-Butadiane-Styrene Fabricated by Fused Deposition Modeling
C. Yen, Army Research Laboratory, Aberdeen, MD; A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI; M. Pankow, Army Research Laboratory, Aberdeen, MD
1130 hrs AIAA-2012-1572 Deformation Response of Hybrid 3D Woven Composites
1030 hrs AIAA-2012-1575 Performance of Composite Materials Subjected to Salt Water Environments
Wind Turbine Composite Material Testing
J. Riddick, Army Research Laboratory, Aberdeen Proving Ground, MD; A. Hall, D. Carponcin, French Space Agency (CNES), Motile Robotics, Inc., Joppa, MD; M. Haile, Toulouse, France; E. Dantras, J. Dandurand, Army Research Laboratory, Aberdeen Proving C. Lacabanne, L. Laffont, National Center for Ground, MD; D. Cole, Motile Robotics, Inc., Scientific Research (CNRS), Toulouse, France; Joppa, MD; R. Von Wahlde, Army Research L. Cadièrgues, French Space Agency (CNES), Laboratory, Aberdeen Proving Ground, MD; S. Toulouse, France; G. Aridon, F. Levallois, EADS, Biggs, Motile Robotics, Inc., Joppa, MD Toulouse, France
D. Miller, J. Mandell, D. Samborsky, L. Cormier, University of Québec, Montréal, Montana State University, Bozeman, MT; Canada; R. Nijssen, S. Raijmaekers, Wind D. Griffith, Sandia National Laboratories, Albuquerque, NM Turbine Materials and Constructions, Wieringerwerf, The Netherlands
1000 hrs AIAA-2012-1574 Temperature and Frequency Effects on the Fatigue Properties of Unidirectional Glass Fiber-Epoxy Composites
M. Bonakdar, G. Seidel, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Inman, University of Michigan, Ann Arbor, Ann Arbor, MI
1100 hrs AIAA-2012-1825 Effect of Nanoscale Fillers on the Viscoelasticity of Polymer Nanocomposites
Nanostructured Materials II
Composite Processes and Characterization
Chaired by: D. POWELL, Southern Research Institute and A. KELKAR, North Carolina A&T State University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1568 AIAA-2012-1569 AIAA-2012-1570 Scaling Challenges Encountered Influence of Vacuum and Processing and Characterization of a with Out-of-Autoclave Prepregs Temperature During Simulated Submicronic Ceramic-Thermoplastic T. Centea, S. Hughes, S. Payette, J. Kratz, Aging on Properties of a Polyepoxy Polymer Composite: Particle Size and P. Hubert, McGill University, Montréal, Adhesive Used in Spacecraft Volume Fraction Optimization for Canada Applications Promoting a Smart and Lightweight N. Causse, E. Dantras, National Center Piezoelectric Material for Space for Scientific Research (CNRS), Toulouse, Applications
Tuesday, 24 April 2012 51-SDM-36
S. Wicks, S. Kalamoun, M. Williams, University of Pennsylvania, Philadelphia, R. Guzman de Villoria, Massachusetts Institute R. Guzman de Villoria, B. Wardle, Philadelphia, PA; K. Takahashi, University of of Technology, Cambridge, MA; L. Ydrefors, Massachusetts Institute of Technology, California, Los Angeles, Los Angeles, CA; H. Cambridge, MA P. Hallander, Saab, Linköping, Sweden; Cebeci, M. Williams, E. Parsons, S. Socrate, B. K. Ishiguro, Massachusetts Institute of Wardle, Massachusetts Institute of Technology, Technology, Cambridge, MA; P. Nordin, Saab, Cambridge, MA Linköping, Sweden; B. Wardle, Massachusetts Institute of Technology, Cambridge, MA
Chaired by: G. ODEGARD and E. GLAESSGEN, NASA Langley Research Center 0930 hrs 1000 hrs AIAA-2012-1565 AIAA-2012-1566 Elastic Properties of Aligned Carbon Aligned Carbon Nanotube Nanotube Polymer Nanocomposites Reinforcement of Aerospace Carbon Fiber Composites: with Controlled Morphology R. Guzman de Villoria, Massachusetts Institute Substructural Strength Evaluation of Technology, Cambridge, MA; S. Chan, for Aerostructure Applications
Tuesday, 24 April 2012 50-SDM-35
Kahuku
Kohala
Waimea Canyon
27
Q. Wang, W. Yu, Utah State University, Logan, UT
N. Katsumata, M. Natori, H. Yamakawa, Waseda University, Tokyo, Japan
L. Stiles, H. Schaub, University of Colorado, Boulder, Boulder, CO
Novel Applications and Innovations
D. Widana-Gamage, R. Jha, Clarkson University, Potsdam, NY; G. Srinivasan, Indian Institute of Science, Bangalore, India
1630 hrs AIAA-2012-1579 Wavelet spectral finite element modeling of transverse crack for structural health monitoring of composite plates
Composite Structures Applications
T. Simpson, Pennsylvania State University, University Park, PA; J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI
University of Victoria, Victoria, Canada
P. Dunning, H. Kim, University of Bath, Bath, United Kingdom
1630 hrs AIAA-2012-1588 Robust Topology Optimisation for Expected Compliance and Variance Using Level-Set Method
J. Martins, J. Hwang, University of Michigan, Ann Arbor, Ann Arbor, MI
1700 hrs AIAA-2012-1589 Review and Unification of Methods for Computing Derivatives of Multidisciplinary Systems
Special Session: MDO Past, Present, Future
Chaired by: K. WILLCOX, Massachusetts Institute of Technology and A. SULEMAN, University of Victoria 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1586 AIAA-2012-1587 AIAA-2012-1585 A Standard Platform for Testing of Robust and Reliability Based Design Advancing the Design of Complex MDAO Architectures Optimization Framework for Wing Engineered Systems through Multidisciplinary Design Optimization: J. Gray, C. Heath, K. Moore, NASA Glenn Design Research Center, Cleveland, OH A. Suleman, C. Crawford, R. Paiva, Report from an NSF Workshop
Tuesday, 24 April 2012 56-MDO-8
1700 hrs AIAA-2012-1908 EM Analysis of a Deployable Composite Shell Reflector for Space Applications
H. Monner, German Aerospace Center (DLR), Braunschweig, Germany
1700 hrs AIAA-2012-1580 Groundtest of a Composite Smart Droop Nose
M. Wiedemann, German Aerospace Center D. Doyle, J. Banik, B. Arritt, Air Force (DLR), Braunschweig, Germany Research Laboratory, Kirtland AFB, NM
Chaired by: L. DATASHVILI, Technical University of Munich and P. TARAZAGA, Virginia Polytechnic Institute and State University 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2012-1581 AIAA-2012-1582 AIAA-2012-1583 AIAA-2012-1584 MegaFlex - The Scaling Potential of Experimental and Theoretical Electron Flux Deflection A New Deployable Truss for UltraFlex Technology Evaluations on Deployment Behavior Experiments with Coulomb Gossamer Space Structures D. Murphy, ATK, Goleta, CA M. Hillebrandt, M. Straubel, C. Huehne, of Inflatable Boom Elements Gossamer Structures
Tuesday, 24 April 2012 55-GSF-2
United Kingdom; M. Santer, Imperial London, London, United Kingdom College London, London, United Kingdom; A. Pirrera, P. Weaver, University of Bristol, Bristol, United Kingdom
NDA Keynote Uncertainty Quantification in System Risk Assessment and Decision-Making Professor Sankaran Mahadevan John R. Murray Sr. Chair in Engineering Vanderbilt University, Nashville, TN
Chaired by: D. AMBUR, NASA Langley Research Center and R. JHA, Clarkson University 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1576 AIAA-2012-1577 AIAA-2012-1578 Pseudo-Bistable Morphing Aeroelastic Optimization of a Multiphysics Modeling of Composite Composites Morphing 2D Shock Control Bump Beams under Large Temperature A. Brinkmeyer, University of Bristol, Bristol, O. Rhodes, M. Santer, Imperial College Changes
Tuesday, 24 April 2012 54-ASC-2
Tuesday, 24 April 2012 53-NDA-6 1330 - 1430 hrs
G. Cheng, G. Wang, Simon Fraser University, Surrey, Canada
1730 hrs AIAA-2012-1590 Trust Region Based MPS Method for Global Optimization of High Dimensional Design Problems
R. Orszulik, J. Shan, York University, Toronto, Canada
1730 hrs AIAA-2012-1920 A Simple PI Controller for Active Flatness and Tracking Control of a Space Membrane Structure
Niihau
Honolulu
Oahu
Kauai
28
K. Hu, L. Swiler, A. Urbina, Sandia National Laboratories, Albuquerque, NM
C. Park, N. Kim, R. Haftka, University of Florida, Gainesville, Gainesville, FL
1530 hrs AIAA-2012-1592 Estimating Probability of Failure of Composite Laminated Panel with Multiple Failure Modes R. Navaid, S. Venkataraman, San Diego State University, San Diego, CA
1630 hrs AIAA-2012-1594 Variance Sensitivity Analysis of Parameters in Puck’s Failure Theory for Composites
Madison, WI; S. Lacy, Air Force Research Laboratory, Kirtland AFB, NM; V. Babuska, Sandia National Laboratories, Albuquerque, NM; S. Lane, Air Force Research Laboratory, Kirtland AFB, NM; T. Paez, MannaTech Engineering, Albuquerque, NM
1630 hrs AIAA-2012-1603 High-Fidelity Total-Lagrangian Geometrically Exact Modeling and Analysis of Highly Flexible Plates/ Shells
Shells and Pressure Vessels
D. Sparkman, H. Millwater, University of Texas, San Antonio, San Antonio, TX; P. Golden, R. John, Air Force Research Laboratory, Wright-Patterson AFB, OH
1630 hrs AIAA-2012-1599 Probabilistic Framework for Prediction of Material Property Distributions from Small D. Krattiger, University of Wisconsin, Madison, Microstructural Models
1600 hrs AIAA-2012-1598 Data-Based Stochastic Evaluation of Closed-Loop Stability and Performance Metrics
F. Gern, NASA Langley Research Center, Hampton, VA
1630 hrs AIAA-2012-1610 Survey of Reliability Analysis Methods for Design Optimization of Aircraft Structures
1700 hrs AIAA-2012-1611 The design and flight test of a new smart wing system
T. Williams, Los Alamos National Laboratory, Los Alamos, NM
1700 hrs AIAA-2012-1604 A New Theoretical Framework for the Formulation of General, Nonlinear, Multiscale Shell Theories
V. Shanmugam, Wright State University, Dayton, OH; R. Penmetsa, E. Tuegel, S. Clay, Air Force Research Laboratory, Wright-Patterson AFB, OH
1700 hrs AIAA-2012-1940 Probabilistic Cohesive Zone Model to Capture Steady State Energy Release Rate Variations of DCB Specimens
Y. Wang, Beihang University, Beijing, T. Richardson, The Boeing Company, Saint N. Di Matteo, S. Guo, R. Morishima, Cranfield J. Diaz, S. Hernandez, L. Romera, A. Baldomir, China Louis, MO University, Cranfield, United Kingdom University of Coruna, La Coruna, Spain
Chaired by: M. MOHAGHEGH, The Boeing Company and B. BEDNARCYK, NASA Glenn Research Center 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1607 AIAA-2012-1609 AIAA-2012-1606 Phantom Eye - Accelerated Air Optimization of Leading Edge and Finite Element Based HWB Flap with Actuation System for a Centerbody Structural Optimization Vehicle Structural Development thru Prototyping Variable Camber Wing and Weight Prediction
Aircraft Design
P. Gustafson, Western Michigan University, P. Gustafson, Western Michigan University, D. Crisafulli, Centre de Recherche Public Kalamazoo, MI Kalamazoo, MI Henri Tudor, Esch-sur-Alzette, Luxembourg; P. Pai, University of Missouri, Columbia, M. Cinefra, E. Carrera, Technical University Columbia, MO of Turin, Turin, Italy
Tuesday, 24 April 2012 60-SDM-39
E. Paulson, Air Force Research Laboratory, Edwards AFB, CA; R. Starkey, University of Colorado, Boulder, Boulder, CO
1700 hrs AIAA-2012-1595 Revisions to the Multistage Reliability-Based Design Optimization Method
Engineering Applications of Non-Deterministic Approaches I
X. Guan, J. He, R. Jha, Y. Liu, Clarkson University, Potsdam, NY
1600 hrs AIAA-2012-1593 Time-dependent reliability analysis using efficient Bayesian method
Failure Analysis and Realability Assessment
Chaired by: B. WILLIS, The Boeing Company and B. WARDLE, Massachusetts Institute of Technology 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1601 AIAA-2012-1602 AIAA-2012-1600 Optimal Wrap Angles for Composite Optimal Wrap Angles for Composite Advanced Layer-Wise Shells Pressure Vessels Part 1: Static Pressure Vessels Part 2: Dynamic Theories Based on Trigonometric Orthogonal Arrays Failure Modes Functions Expansion
Tuesday, 24 April 2012 59-SDM-38
S. Pattabhiraman, University of Florida, Gainesville, Gainesville, FL; C. Gogu, Paul Sabatier University, Toulouse, France; N. Kim, R. Haftka, University of Florida, Gainesville, Gainesville, FL; C. Bes, Paul Sabatier University, Toulouse, France
Chaired by: V. ROMERO, Sandia National Laboratories and S. SCOTTI 1500 hrs 1530 hrs AIAA-2012-1596 AIAA-2012-1597 Synchronizing Condition-based Bayesian Model Selection Between Maintenance with Necessary Underdetermined Nuclear Reactor Scheduled Maintenance Models
Tuesday, 24 April 2012 58-NDA-8
J. Patel, S. Choi, Georgia Institute of Technology, Atlanta, GA
Chaired by: G. MODGIL 1500 hrs AIAA-2012-1591 Advanced Probabilistic Neural Network for Reliability Estimation via Semi-supervised Learning
Tuesday, 24 April 2012 57-NDA-7
G. Hrinda, NASA Langley Research Center, Hampton, VA
1730 hrs AIAA-2012-1605 Effects of Shell-Buckling Knockdown Factors in Large Cylindrical Shells
C. Chamis, NASA Glenn Research Center, Cleveland, OH
1730 hrs AIAA-2012-1941 Probabilistic Simulation of MultiScale Multi-Functional Composite Behavior
Waimea Canyon
Kona
Kauai
Hilo
29
Hampton, VA; K. Karayev, The Boeing Company, Seattle, WA
Center, Huntsville, AL; B. LaVerde, ERC, Inc., M. Morton, J. Cox, Lockheed Martin Corporation, Marietta, GA; E. Powell, Self, Huntsville, AL; R. Hunt, Triumph Aerospace, Huntsville, AL; C. Fulcher, R. Towner, E. Marietta, GA McDonald, Jacobs, Huntsville, AL
Chaired by: V. BABUSKA and R. LIND, University of Florida 1530 hrs 1500 hrs AIAA-2012-1625 AIAA-2012-1624 Calculation of Coupled Initial Assessment of a CFD Application for Predicting Jet Vibroacoustics Response Estimates Fighter Aircraft Cavity Bay from a Library of Available Uncoupled Transfer Function Sets Acoustics for Subsonic and A. Smith, J. Peck, NASA Marshall Space Flight Supersonic Aircraft States
Tuesday, 24 April 2012 63-SDM-42
D. Kenik, E. Nelson, Firehole Composites, Laramie, WY; G. Mabson, The Boeing Company, Seattle, WA
1630 hrs AIAA-2012-1627 Multi-objective Vibro-acoustic Optimization of Point Excited Curved Panels with Straight/ Curvilinear Stiffeners
VibroAcoustics
S. Liguore, D. Pitt, M. Thomas, The Boeing P. Joshi, S. Mulani, R. Kapania, Virginia Company, Saint Louis, MO; L. Shaw, Polytechnic Institute and State University, Air Force Research Laboratory, WrightBlacksburg, VA Patterson AFB, OH
1600 hrs AIAA-2012-1626 Application and Demonstration of Nonlinear Reduced Order Modeling (NLROM) for Thermal/Acoustic Response
N. Muraliraj, The Boeing Company, Everett, WA; T. Walker, NSE Composites, Seattle, WA; E. Nelson, D. Robbins, D. Kenik, Firehole Composites, Laramie, WY
J. Parmigiani, T. Kennedy, T. Wright, Oregon State University, Corvallis, OR
1630 hrs AIAA-2012-1621 Mesh Dependency in Progressive Failure Modeling of Notched Laminates Under Out-of-Plane Bending
M. Swindeman, University of Dayton Research Institute, Dayton, OH; D. Mollenhauer, Air Force Research Laboratory, Wright-Patterson AFB, OH; R. Brockman, E. Iarve, University of Dayton Research Institute, Dayton, OH
1730 hrs AIAA-2012-1623 Mesh Dependence of the Discrete Damage Modeling in Laminated Composites
1700 hrs AIAA-2012-1628 Validation of Component Vibrations Predicted from Response Matching Method by Finite Element Acoustic Analysis Y. Chung, D. Krebs, H. Tong, The Boeing Company, Huntington Beach, CA; C. Fulcher, Jacobs, Huntsville, AL
G. Mabson, O. Weckner, V. Balabanov, M. Ramnath, The Boeing Company, Seattle, WA
1700 hrs AIAA-2012-1622 Finite Element Based Decohesive Failure Simulation Sensitivity Studies
Mesh Dependence of Failure Predictions
Chaired by: A. WAAS, University of Michigan and G. MABSON, The Boeing Company 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1618 AIAA-2012-1619 AIAA-2012-1620 Developing Guidelines for the Influence of Finite Element Size Energy-Based Stiffness Degradation Application of Coupled Fracture/ in Residual Strength Prediction of for Alleviation of Mesh Sensitivity Continuum Mechanics - Based Composite Structures for Progressive Failure Analysis of A. Satyanarayana, ATK, Hampton, VA; P. Center-Notched Composite Panels Composite Damage Models for Bogert, NASA Langley Research Center, K. Karayev, P. Minguet, S. Lee, V. Balabanov, Reducing Mesh Sensitivity
Tuesday, 24 April 2012 62-SDM-41
E. Pineda, A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI
1700 hrs AIAA-2012-1617 Finite Element Modeling of Z-Pinned Composite Structures under Mode II Loading
H. Kim, G. Defrancisci, Z. Chen, University P. Ranatunga, Miami University, Middletown, of California, San Diego, La Jolla, CA OH; S. Clay, Air Force Research Laboratory, Wright-Patterson AFB, OH
1630 hrs AIAA-2012-1616 Estimation of Ground Service Equipment Contact Damage in Composite Aircraft Panels
Composite Damage and Delamination
Chaired by: C. CHAMIS, NASA Glenn Research Center and A. CHATTOPADHYAY, Arizona State University 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1612 AIAA-2012-1613 AIAA-2012-1614 Analysis Methodology for Assessing A Thermodynamically-Based Mesh Debond Resisting Composite Delaminations in Composite Objective Work Potential Theory for Stringers Overwrapped Pressure Vessels Predicting Intralaminar Progressive M. O’Donnell, P. Weaver, University of Bristol, Bristol, United Kingdom; E. V. Goyal, J. Rome, The Aerospace Damage and Failure in FiberCosentino, Airbus, Bristol, United Kingdom Corporation, El Segundo, CA Reinforced Laminates
Tuesday, 24 April 2012 61-SDM-40
Koko Crater
Lanai
Waianae
30
University, Durham, NC
Hampton, VA
Maryland, College Park, College Park, MD; P. Masarati, Technical University of Milan, Milan, Italy; J. Baeder, I. Chopra, University of Maryland, College Park, College Park, MD; M. Morandini, G. Quaranta, Technical University of Milan, Milan, Italy
E. Musil, A. Evuri, U. Korde, C. Widener, South Dakota School of Mines & Technology, Rapid City, SD
A. Smith, NASA Marshall Space Flight Center, Huntsville, AL; B. LaVerde, ERC, Inc., Huntsville, AL; R. Hunt, Triumph Aerospace, Huntsville, AL; B. Craigmyle, Jacobs, Huntsville, AL
A. Jennings, J. Black, Air Force Institute of Technology, Wright-Patterson AFB, OH; J. Alerding, Virginia Military Institute, Lexington, VA
1600 hrs AIAA-2012-1637 Flapping Wing Force and Deformation Analysis
State University, University Park, PA; V. Babuska, Sandia National Laboratories, Albuquerque, NM
Chaired by: W. WELSH, Sikorsky Aircraft and P. FRIEDMANN, University of Michigan 1530 hrs 1600 hrs 1500 hrs AIAA-2012-1642 AIAA-2012-1643 AIAA-2012-1641 Damping Models for Shear Beams Friction Stir Processing of Validation of Measured Damping with Applications to Spacecraft Aluminum for Enhanced Passive Trends for Flight-Like Vehicle Wiring Harnesses Damping: Modeling and Testing of Panel/Equipment Including a J. Kauffman, G. Lesieutre, Pennsylvania Two Structures Range of Cable Harness Assemblies
Tuesday, 24 April 2012 66-SDM-45
T. Vanneste, J. Paquet, ONERA, Lille, France; S. Grondel, E. Cattan, National Center for Scientific Research (CNRS), Villeneuve d’Ascq, France
Chaired by: R. GORDNIER, Air Force Reseach Laboratory 1500 hrs 1530 hrs AIAA-2012-1635 AIAA-2012-1636 Design of a lift-optimized flapping- CFD-CSD Coupled Aeroelastic Analysis wing using a finite element of Flexible Flapping Wings for MAV aeroelastic framework of insect Applications: Methodology Validation R. Malhan, V. Lakshminarayan, University of flight
Tuesday, 24 April 2012 65-SDM-44
M. Benedict, T. Jarugumilli, I. Chopra, University of Maryland, College Park, College Park, MD
Chaired by: B. WHITING, The Boeing Company and C. HEBERT, Sierra Nevada Corporation 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1629 AIAA-2012-1630 AIAA-2012-1631 Aeroelastic Responses of SpringUncertainty Due to Unsteady Fluid/ Experimental and Computational Structure Interaction for the Ares Studies to Understand the Role of Flow suspended Airfoil Systems in I Vehicle Traversing the Transonic Curvature Effects on the Aerodynamic Transonic Buffeting Flows Performance of a MAV-Scale Cycloidal D. Raveh, Technion--Israel Institute of Regime Technology, Haifa, Israel; E. Dowell, Duke R. Bartels, NASA Langley Research Center, Rotor in Forward Flight
Tuesday, 24 April 2012 64-SDM-43
1700 hrs AIAA-2012-1639 Towards a Fundamental Understanding of Low Reynolds Number Hover-Capable Flapping Wing Aerodynamics
1700 hrs AIAA-2012-1645 A Hysteretic Energy Method for Determining Damping Properties of Hard Coatings
1730 hrs AIAA-2012-1646 Vibration Analysis of A Helicopter Blade with A Piezoelectric Actuated Trailing Edge Flap
J. Min, NASA Glenn Research Center, O. Scott-Emuakpor, B. Runyon, T. George, O. Ozdemir Ozgumus, M. Kaya, Istanbul Cleveland, OH; K. Duffy, University of Air Force Research Laboratory, WrightTechnical University, Istanbul, Turkey Toledo, Cleveland, OH; A. Provenza, NASA Patterson AFB, OH Glenn Research Center, Cleveland, OH
1630 hrs AIAA-2012-1644 Piezoelectric Vibration Damping Study for Rotating Composite Fan Blades
Damping and Vibration Supression
J. Jaworski, University of Cambridge, Cambridge, United Kingdom; R. Gordnier, Air Force Research Laboratory, WrightPatterson AFB, OH
1730 hrs AIAA-2012-1640 Thrust Augmentation of Flapping Airfoils in Low Reynolds Number Flow Using a Flexible Membrane
1730 hrs AIAA-2012-1634 Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
M. Ritter, German Aerospace Center (DLR), P. Mardanpour, D. Hodges, Georgia Göttingen, Germany Institute of Technology, Atlanta, GA; R. Neuhart, N. Graybeal, Bihrle Applied Research, Hampton, VA
1700 hrs AIAA-2012-1633 Static and Forced Motion Aeroelastic Simulations of the HIRENASD Wind Tunnel Model
B. Stanford, P. Beran, R. Snyder, Air Force Research Laboratory, Wright-Patterson AFB, P. Seshadri, M. Benedict, I. Chopra, OH; M. Patil, Virginia Polytechnic Institute and University of Maryland, College Park, State University, Blacksburg, VA College Park, MD
1630 hrs AIAA-2012-1638 Stability and Power Optimality in Time-Periodic Flapping Wing Structures
Micro Air Vehicle Aeroelastics
M. Iovnovich, D. Raveh, Technion--Israel Institute of Technology, Haifa, Israel
1630 hrs AIAA-2012-1632 3D and Finite-wing Effects on the Shock-buffet Instability Mechanism
Aeroelasticity I
Molokai
Waialua
Akaka Falls
31
C. Teng, W. Yu, Utah State University, Logan, UT; M. Chen, Air Force Research Laboratory, Wright-Patterson AFB, OH
Bristol, United Kingdom
Y. Bichiou, M. Ghommem, Virginia Polytechnic CA; K. Van Buren, Clemson University, Institute and State University, Blacksburg, VA; Clemson, SC; F. Hemez, Los Alamos National A. Nuhait, King Saud University, Riyadh, Saudi Laboratory, Los Alamos, NM Arabia; M. Hajj, Virginia Polytechnic Institute and State University, Blacksburg, VA
C. Zhang, Clarkson University, Potsdam, NY; J. Xu, Z. Lu, Beijing Aeronautical Science and Technology Research Institute, Beijing, China; Y. Liu, Clarkson University, Potsdam, NY
1630 hrs AIAA-2012-1653 General Fracture Criterion for Mixed-mode Delamination in Composite Materials E. Saavedra Flores, F. Díaz De la O, M. Friswell, J. Sienz, Swansea University, Swansea, United Kingdom
1700 hrs AIAA-2012-1654 A Multi-scale Finite Element Approach for the Random Mechanical Response of Honeycomb-cored Structures
H. Meidani, R. Ghanem, University of Southern California, Los Angeles, CA
Non-Deterministic Approaches Applied to Wind Energy
D. Mollenhauer, T. Breitzman, Air Force S. Mital, University of Toledo, Toledo, OH; Research Laboratory, Wright-Patterson R. Goldberg, P. Bonacuse, NASA Glenn AFB, OH; E. Iarve, K. Hoos, M. Research Center, Cleveland, OH Swindeman, E. Zhou, University of Dayton Research Institute, Dayton, OH
Chaired by: C. PETTIT, U.S. Naval Academy and M. HAJJ, Virginia Polytechnic Institute and State University 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1655 AIAA-2012-1658 AIAA-2012-1659 Sensitivity to Gust Parameters and Developing Simplified Models for Random Eigenvalues for the Control of Aerodynamic Loads on a Wind Turbine Blades Analysis of Uncertain Turbine M. Mollineaux, Stanford University, Stanford, Blades Rotating Blade
Tuesday, 24 April 2012 69-SDM-48
M. Garnich, R. Fertig, E. Anderson, S. Deng, University of Wyoming, Laramie, Laramie, WY
Multifunctional Materials
Multiscale Modeling of Damage in Composites
Chaired by: G. SEIDEL, Virginia Polytechnic Institute and State University and S. WANTHAL, The Boeing Company 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1650 AIAA-2012-1651 AIAA-2012-1652 Micromechanics of Fatigue Simulation of Mode I Fracture at Modeling of Damage Initiation and Damage in Unidirectional Polymer the Micro-Level in Polymer Matrix Progression in a SiC/SiC Woven Composites Composite Laminate Plies Ceramic Matrix Composite
Tuesday, 24 April 2012 68-SDM-47
G. Lanzara, University of Rome, Rome, Italy; L. Basiricò, Institute of Advanced Technologies, Trapani, Italy
Chaired by: K. SHIVAKUMAR, North Carolina A&T State University and A. AVILA, Federal University of Minas Gerais 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1647 AIAA-2012-1648 AIAA-2012-1649 Autonomous self-healing of Self-Rechargeable Multifunctional Micromechanics Modeling of damaged CFRPs Carbon Fiber Composites with CNTs High Temperature Materials with Temperature-dependent Constituents V. Imperiale, I. Bond, University of Bristol, Supercapacitors
Tuesday, 24 April 2012 67-SDM-46
Kahuku
Maui
Kohala
32
N. Silvernail, Embry-Riddle Aeronautical University, Daytona Beach, FL
W. Vieira, University of São Paulo, São Carlos, B. Natarajan, W. Eun, J. Lee, S. Shin, Seoul Brazil; F. Nitzsche, Carleton University, Ottawa, National University, Seoul, South Korea Canada; C. De Marqui Jr., University of São Paulo, São Carlos, Brazil
K. Patterson, S. Pellegrino, California Institute of Technology, Pasadena, CA
ASC Keynote
Wednesday
J. Lee, Hanyang University, Seoul, South Korea; G. Park, Hanyang University, Ansan, South Korea
1630 hrs AIAA-2012-1663 A Preliminary Study on the Optimum Parameters in Sheet Metal Forming
Design Engineering
B. Youn, Seoul National University, Seoul, South Korea; C. Hu, University of Maryland, College Park, MD; P. Wang, Wichita State University, Wichita, KS
1130 hrs AIAA-2012-1672 Three-Point Suspension for Circular Membrane Apertures
G. Greschik, TentGuild Engineering Company, Boulder, CO G. Greschik, TentGuild Engineering Company, Boulder, CO; A. Palisoc, L’Garde, Inc., Tustin, CA
1100 hrs AIAA-2012-1671 CubeSat-Deployable Photon Sieve Design for Strength and a High Level of Deployment Control
Deployable Apertures - Optics
S. Daynes, P. Weaver, University of Bristol, Bristol, United Kingdom
1100 hrs AIAA-2012-1667 Morphing Blade Fluid-Structure Interaction
Rotorcraft Applications
1700 hrs AIAA-2012-1811 Resilience Allocation for Engineered System Design
Adaptive Structures: The Journey to Flight George A. Lesieutre Professor and Head, Aerospace Engineering Pennsylvania State University
1030 hrs AIAA-2012-1670 MOIRE Gossamer Space Telescope Structural Challenges and Solutions
F. Grobler, A. Gubel, E. Meehan, T. Tibbets, W. Tandy, P. Atcheson, J. Domber, A. C. Jenkins, Montana State University, Seltzer, Ball Aerospace & Technologies, Bozeman, MT; K. Woo, Chungbuk National Corporation, Boulder, CO University, Chongju, South Korea
Chaired by: H. FANG and M. SANTER, Imperial College London 1000 hrs 0930 hrs AIAA-2012-1669 AIAA-2012-1668 Magnetically-Controlled Membrane Thin deformable mirrors for a Reflector reconfigurable space telescope
Wednesday, 25 April 2012 73-GSF-3
R. Vocke, University of Maryland, College Park, College Park, MD; C. Kothera, Techno-Sciences, Inc., Beltsville, MD; N. Wereley, University of Maryland, College Park, College Park, MD
Chaired by: I. CHOPRA, University of Maryland and N. WERELEY, University of Maryland 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1665 AIAA-2012-1666 AIAA-2012-1664 Modeling and Analysis of Structural Design of an Active Development of a SpanTrailing-Edge Flap Blade for Extending Blade Tip System for a Piezoelectric Energy Harvesting from Helicopter Blades Helicopter Vibration Control Reconfigurable Helicopter Rotor
Wednesday, 25 April 2012 72-ASC-4
Wednesday, 25 April 2012 71-ASC-3 0800 - 0900 hrs
Sapporo, Japan M. Henke, M. Biester, Leibniz University of Hannover, Hannover, Germany; Y. Guendogdu, MTU Aero Engines, Munich, Germany; J. Seume, Leibniz University of Hannover, Hannover, Germany; F. Lippl, E. Mass, MTU Aero Engines, Munich, Germany
Chaired by: G. BROWN, The Boeing Company and G. HONEA, Raytheon Company 1500 hrs 1530 hrs 1600 hrs AIAA-2012-1660 AIAA-2012-1661 AIAA-2012-1662 On the Approximate Bending Investigation to Determine Numerical assisted Design of a Variable Rotating Vane Carrier Device Stiffness for Structural Optimization Rotational Stability of On-Orbit Propellant Storage and Transfer for Turbine Test Rigs with split Housing of Double-skin Hollowed Structures using a Segmented Half- Rectangular Plates Systems Undergoing Operational Y. Ohta, Hokkaido Institute of Technology, Fuel Transfer Scenarios Ring Bearing Concept
Tuesday, 24 April 2012 70-SDM-49
Honolulu
Oahu
Kauai
Puna
33
Bath, Bath, United Kingdom
P. Congedo, National Institute for Research in Computer Science and Control, Bordeaux, France; G. Iaccarino, J. Witteveen, Stanford University, Stanford, CA
M. Hilburger, NASA Langley Research Center, Hampton, VA
Hampton, VA; P. Chunchu, Eagle Aeronautics, Inc., Hampton, VA; A. Satyanarayana, ATK, Hampton, VA; M. Hilburger, R. Smith, NASA Langley Research Center, Hampton, VA
A. Chaudhuri, R. Haftka, F. Viana, University of Florida, Gainesville, FL
1100 hrs AIAA-2012-1681 Efficient Global Optimization with Adaptive Target for Probability of Targeted Improvement
Optimization Methods
S. Rangavajhala, C. Liang, S. Mahadevan, V. Hombal, Vanderbilt University, Nashville, TN
M. Hilburger, W. Haynie, A. Lovejoy, NASA Langley Research Center, Hampton, VA; W. Waters, H. Herring, Lockheed Martin Corporation, Hampton, VA
W. Haynie, M. Hilburger, NASA Langley Research Center, Hampton, VA; M. Bogge, M. Maspoli, Technical University of Turin, Turin, Italy; B. Kriegesmann, Leibniz University of Hannover, Hannover, Germany
1100 hrs AIAA-2012-1689 Validation of Lower-Bound Estimates for Compression-Loaded Cylindrical Shells
M. Schultz, C. Rose, NASA Langley Research Center, Hampton, VA; J. Guzman, D. McCarville, The Boeing Company, Seattle, WA; M. Hilburger, NASA Langley Research Center, Hampton, VA
1130 hrs AIAA-2012-1690 Experimental Study of the Compression Response of FlutedCore Composite Panels with Joints
Developing the Next Generation of Shell Buckling Design Factors and Technologies I - Testing
C. Pettit, U.S. Naval Academy, Annapolis, MD; S. Vecherin, D. Wilson, Army Corps of Engineers, Hanover, NH
1030 hrs AIAA-2012-1685 Sensitivity Analysis of QuasiWavelet Models of Heterogeneous Materials
1130 hrs AIAA-2012-1682 Concurrent optimization of mesh refinement and design parameters in multidisciplinary design
Development of Non-Deterministic Methods I
Chaired by: M. HILBURGER, NASA Langley Research Center and A. LOVEJOY, NASA Langley Research Center 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1687 AIAA-2012-1688 AIAA-2012-1686 Test and Analysis of Sub-Components Sub-Scale and Full-Scale Testing Developing the Next Generation Shell Buckling Design Factors and of Aluminum-Lithium Alloy Cylinders of Buckling-Critical Launch Vehicle W. Haynie, NASA Langley Research Center, Shell Structures Technologies
Wednesday, 25 April 2012 77-SDM-50
J. Witteveen, G. Iaccarino, Stanford University, Stanford, CA
Chaired by: M. ELDRED, Sandia National Laboratories 0930 hrs 1000 hrs AIAA-2012-1683 AIAA-2012-1684 Robust Uncertainty Quantification A simplex-simplex approach based on Essentially Nonfor mixed aleatory-epistemic Oscillatory Stencil Selection uncertainty quantification
Wednesday, 25 April 2012 76-NDA-9
Polytechnic Institute, Troy, NY; A. Messac, S. Hernandez, A. Baldomir, J. Diaz, Syracuse University, Syracuse, NY University of Coruna, A Coruna, Spain
T. Kipouros, Cambridge University, Cambridge, United Kingdom; T. Peachey, D. Abramson, Monash University, Melbourne, Australia; A. Savill, Cranfield University, Cranfield, United Kingdom
1130 hrs AIAA-2012-1677 Enhancing and Developing the Practical Optimisation Capabilities and Intelligence of Automatic D. Locatelli, S. Mulani, R. Kapania, Virginia Design Software
1100 hrs AIAA-2012-1676 A Multidisciplinary Analysis Optimization Environment for Wings Having SpaRibs
Optimization Frameworks
K. Risse, E. Anton, T. Lammering, K. Franz, R. Hoernschemeyer, RWTH Aachen Polytechnic Institute and State University, University, Aachen, Germany Blacksburg, VA; P. Chen, D. Sarhaddi, ZONA Technology, Inc., Scottsdale, AZ
Chaired by: S. MISSOUM, University of Arizona and P. ROHL, Advatech Pacific, Inc. 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1678 AIAA-2012-1679 AIAA-2012-1680 Avoiding Premature Convergence A Unified Approach of Optimality Geometric Programming for in a Mixed-Discrete Particle Swarm Criteria and Mathematical Aircraft Design Optimization W. Hoburg, P. Abbeel, University of Optimization (MDPSO) Algorithm Programming via the Maximum California, Berkeley, Berkeley, CA S. Chowdhury, J. Zhang, Rensselaer Entropy Method
Wednesday, 25 April 2012 75-MDO-10
C. Heath, J. Gray, NASA Glenn Research Center, Cleveland, OH
Chaired by: H. KIM, University of Bath and E. ALYANAK, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1673 AIAA-2012-1674 AIAA-2012-1675 A Resource-Oriented Architecture An Integrated Environment for OpenMDAO: Framework for Preliminary Aircraft Design and Flexible Multidisciplinary Design, for MDO Framework Analysis and Optimization Methods K. Duan, H. Kim, J. Padget, University of Optimization
Wednesday, 25 April 2012 74-MDO-9
Lanai
Kauai
Niihau
Hilo
34
Fatigue and Fracture Mechanics III 1100 hrs AIAA-2012-1699 Improved Stress Intensity Factor Solution for Cracks in Panels with Arbitrarily Located Stringers
Chaired by: S. BECZ, Lenze and I. RAJU, NASA Langley Research Center 0930 hrs 1000 hrs AIAA-2012-1696 AIAA-2012-1697 Design and Experimental Validation Crack Growth and Residual of a Mixed-Mode Crack Arrest Strength Prediction of Thin-Walled Specimen Aluminum Structures Using XSHELL
S. Yabili, University of Liège, Liège, Belgium; T. Perry, M. Smith, Georgia Institute of Technology, Atlanta, GA; G. Dimitriadis, University of Liège, Liège, Belgium
Chaired by: T. ROSE 0930 hrs AIAA-2012-1706 Computational Considerations for the Prediction of Stall Flutter
Wednesday, 25 April 2012 81-SDM-54
J. Wang, Shanghai Jiao Tong University, Shanghai, China; A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI; H. Wang, Shanghai Jiao Tong University, Shanghai, China
M. Boscolo, City University London, London, United Kingdom; X. Zhang, Cranfield University, Cranfield, United Kingdom
F. Sabri, S. Meguid, University of Toronto, Toronto, Canada; A. Lakis, École Polytechnique de Montréal, Montréal, Canada
1000 hrs AIAA-2012-1707 Modeling Flutter Response of a Flexible Morphing Wing for UAV
State University, San Diego, CA
T. Skujins, C. Cesnik, University of Michigan, Ann Arbor, Ann Arbor, MI
1030 hrs AIAA-2012-1708 Toward an Unsteady Aerodynamic ROM for Multiple Mach Regimes
S. Marques, Queen’s University Belfast, Belfast, United Kingdom; K. Badcock, University of Liverpool, Liverpool, United Kingdom
1100 hrs AIAA-2012-1709 Impact of Structural Variability on Robust Flutter Optimization
Flutter I
1100 hrs AIAA-2012-1704 Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 2: Analysis
Sandwich Structures
Y. Bombardier, M. Liao, G. Renaud, National Research Council Canada, Ottawa, Canada
K. Lai, K. Lum, National University of Singapore, Singapore, Singapore
1130 hrs AIAA-2012-1710 Flutter-Boundary Prediction Using System Identification-Based Reduced-Order Aeroelasticity Analysis
1130 hrs AIAA-2012-1705 A Refined Zigzag Theory for Laminated Composite and Sandwich Plates Incorporating Thickness Stretch Deformation
G. Renaud, M. Liao, National Research Council Canada, Ottawa, Canada
1130 hrs AIAA-2012-1700 Improved Stress Intensity Factor Solutions for Surface and Corner Cracks at a Hole
D. Robbins, Firehole Composites, Laramie, WY
1130 hrs AIAA-2012-1695 Fiber-Aligned, Discrete-Layer Modeling Approaches for Progressive Failure Simulation of Open Hole Composite Panels
T. McQuigg, R. Kapania, Virginia Polytechnic Institute and State University, A. Barut, E. Madenci, University of Arizona, T. McQuigg, R. Kapania, Virginia Polytechnic Institute and State University, Blacksburg, VA; S. Scotti, S. Walker, NASA Tucson, Tucson, AZ; A. Tessler, NASA Langley Blacksburg, VA; S. Scotti, S. Walker, NASA Langley Research Center, Hampton, VA Research Center, Hampton, VA Langley Research Center, Hampton, VA
1030 hrs AIAA-2012-1703 Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 1: J. Stromsoe, S. Venkataraman, San Diego Experiments
Chaired by: J. ROME, The Aerospace Corporation and M. WOLFF 0930 hrs 1000 hrs AIAA-2012-1701 AIAA-2012-1702 Experimental Study on the LowFunctionally Grading Honeycomb velocity Impact Behavior of Foam- Core Material by Inplane Crushing core Sandwich Panels for Tapered Sandwich Closures
Wednesday, 25 April 2012 80-SDM-53
E. Bruun, K. Lin, University of Washington, J. Lua, L. Liu, Global Engineering and Seattle, Seattle, WA Materials, Inc., Princeton, NJ; J. Chessa, University of Texas, El Paso, El Paso, TX; S. Peng, Northwestern University, Evanston, IL
1030 hrs AIAA-2012-1698 Bonded crack retarders for aircraft integral metallic structures: a sensitivity analysis of design parameters
A. Khan, E. Johnson, R. Kapania, R. Batra, P. Schubel, V. Goyal, J. Rome, D. Patel, Virginia Polytechnic Institute and State G. Steckel, The Aerospace Corporation, El University, Blacksburg, VA; J. Guimard, Segundo, CA EADS, Suresnes, France
Wednesday, 25 April 2012 79-SDM-52
Arizona, Tucson, Tucson, AZ
1100 hrs AIAA-2012-1694 Identification of Failure Mechanisms in Sandwich Structures with Foam Core Thickness Mismatches
Chaired by: R. SHAH, The Boeing Company and R. KOCH, Naval Undersea Warfare Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1691 AIAA-2012-1692 AIAA-2012-1693 Peridynamics for Failure Prediction Progressive Failure Analysis of A Component-Wise Approach for Laminated Composite Structures the Failure Analysis of Composite in Composites E. Oterkus, E. Madenci, University of Based on Puck’s Failure Criteria Structures
E. Carrera, M. Maiarù, M. Petrolo, Technical University of Turin, Turin, Italy
Failure Analysis and Prediction I
Wednesday, 25 April 2012 78-SDM-51
Molokai
Kona
Waialua
Waianae
35
W. Su, C. Cesnik, University of Michigan, Ann Arbor, Ann Arbor, MI
Canada; T. Aarons, J. Garnand-Royo, C. of Engineering, Needham, MA Woolsey, R. Canfield, Virginia Polytechnic Institute and State University, Blacksburg, VA; A. Suleman, University of Victoria, Victoria, Canada
Z. Sotoudeh, Georgia Institute of Technology, Atlanta, GA; A. Ricciardi, R. Canfield, M. Patil, Virginia Polytechnic Institute and State University, Blacksburg, VA
1030 hrs AIAA-2012-1717 A Hybrid Quasi-steady CFD-Inflow Approach for Gust Response Analysis of Highly Flexible Aircraft
B. Ashrafi, M. Jakubinek, Y. Martinez-Rubi, E. Glaessgen, E. Saether, J. Hochhalter, A. Johnston, B. Simard, National Research NASA Langley Research Center, Hampton, Council Canada, Ottawa, Canada VA; V. Gupta, National Institute of Aerospace, Hampton, VA; S. Smith, NASA Langley Research Center, Hampton, VA
D. Kim, Y. Kim, Gyeongsang National University, Jinju, South Korea
A. Bandyopadhyay, G. Odegard, Michigan Technological University, Houghton, MI
E. Stewart, M. Patil, R. Canfield, Virginia Polytechnic Institute and State University, Blacksburg, VA; R. Snyder, Air Force Research Laboratory, Wright-Patterson AFB, OH
1130 hrs AIAA-2012-1724 Aeroelastic Shape Optimization of Micro Air Vehicle Wings
1130 hrs AIAA-2012-1729 Molecular Modeling of the Influence of Crosslink Distribution C. Jang, T. Lacy, S. Gwaltney, C. Pittman, on Epoxy Polymers
1100 hrs AIAA-2012-1728 Molecular dynamics simulation of vinyl ester resin crosslinking
Nanostructured Materials III
M. Ferraro, D. Gorissen, J. Scanlan, A. Keane, E. Quaranta, B. Schumann, J. van Schaik, M. Bolinches i Gisbert, University of Southampton, Southampton, United Kingdom
1100 hrs AIAA-2012-1723 Toward Value-Driven Design of a Small, Low-Cost UAV
Design, Micro/Unmanned Aircraft
Angeles, Los Angeles, CA
1130 hrs AIAA-2012-1719 Transonic Flutter Analysis Using Coupled CFD-CSD Analysis and New O. Bendiksen, University of California, Los Reduced Order Modeling Technique
1100 hrs AIAA-2012-1718 Transonic Stabilization Laws for Unsteady Aerodynamics and Flutter
H. Toghiani, Mississippi State University, Mississippi State, MS S. Sihn, University of Dayton Research Institute, Dayton, OH; V. Varshney, Universal Technology Corporation, Dayton, OH; A. Roy, B. Farmer, Air Force Research Laboratory, Wright-Patterson AFB, OH
Chaired by: B. WARDLE, Massachusetts Institute of Technology and S. ROY, University of Alabama 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1726 AIAA-2012-1727 AIAA-2012-1725 Multiscale Modeling of Structurally- Prediction of Coefficients of A Comparative Study on Thermal Expansion of 3-D CNTMechanical and Electrical Properties Graded Materials Using Discrete Graphene Junctioned Carbon of SWCNT-Modified Epoxy Resins Dislocation Plasticity Models and Continuum Crystal Plasticity Models Nanostructures and Their End-Use Applications
Wednesday, 25 April 2012 85-SDM-58
V. Hrishikeshavan, J. Black, I. Chopra, University of Maryland, College Park, College Park, MD
Chaired by: E. ALTHOF, Raytheon Company and M. BAILEY, General Electric Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1720 AIAA-2012-1721 AIAA-2012-1722 Design and Testing of a Quad Airworthiness Evaluation of a A Perching Landing Gear for a Shrouded Rotor Micro Air Vehicle Scaled Joined-Wing Aircraft Quadcopter J. Richards, University of Victoria, Victoria, E. Culler, C. Lee, Franklin W. Olin College in Hover
Wednesday, 25 April 2012 84-SDM-57
R. Voss, R. Thormann, German Aerospace J. Azevedo, Technological Institute of Center (DLR), Göttingen, Germany Aeronautics (ITA), São José dos Campos, Brazil; J. Azevedo, R. Silva, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil
Chaired by: R. GORDNIER, Air Force Reseach Laboratory 0930 hrs 1000 hrs AIAA-2012-1715 AIAA-2012-1716 Flutter Computations for a Generic Efficient Calculation of Reference Aircraft Adopting CFD Aerodynamic States for Aeroelastic and Reduced Order Methods Analyses in the Frequency Domain
K. Ide, T. Aoki, University of Tokyo, Tokyo, Japan
Computational Aeroelasticity II
Pennsylvania State University, University Park, PA
Wednesday, 25 April 2012 83-SDM-56
Oklahoma, Norman, Norman, OK
1100 hrs AIAA-2012-1714 Amplication of Initial Imperfection of an Ultra-long Beam under Impulsive Compression
Beam Dynamics I
Chaired by: J. KOSMATKA, University of California, San Diego and F. NITZSCHE, Carleton University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1711 AIAA-2012-1712 AIAA-2012-1713 Energy Dissipation of a Bi-stable von- Strain-Based Analysis for Subgrid-scale dynamics for a Mises Truss under Harmonic Excitation Geometrically Nonlinear Beams: A nonlinear beam A. Labryer, P. Attar, P. Vedula, University of S. Barbarino, M. Pontecorvo, F. Gandhi, Modal Approach
Wednesday, 25 April 2012 82-SDM-55
Waimea Canyon
Puna
Koko Crater
Akaka Falls
36
Heverlee, Belgium; F. Vanhollebeke, Hansen Transmissions International, Kontich, Belgium; W. Desmet, Catholic Univerity of Leuven, Heverlee, Belgium
Z. Lu, J. Xu, Beijing Aeronautical Science and Technology Research Institute, Beijing, China; Y. Liu, Clarkson University, Potsdam, NY
Wednesday, 25 April 2012 88-LNCH-1 1200 - 1400 hrs
T. Pahn, Leibniz University of Hannover, Hannover, Germany; J. Jonkman, National Renewable Energy Laboratory, Golden, CO; R. Rolfes, Leibniz University of Hannover, Hannover, Germany; A. Robertson, National Renewable Energy Laboratory, Golden, CO
Chaired by: L. MANUEL, University of Texas, Austin and I. PROWELL 0930 hrs 1000 hrs AIAA-2012-1735 AIAA-2012-1736 Inverse load calculation of wind How the upscaling trend in wind turbine support structures - a turbine design affects dynamic numerical verification using the behaviour of the drive train comprehensive simulation code FAST J. Helsen, Catholic Univerity of Leuven,
Wednesday, 25 April 2012 87-SDM-60
University, Mississippi State, MS; H. Hilton, University of Illinois, Urbana-Champaign, Urbana, IL; D. Drake, Mississippi State University, Mississippi State, MS S. Spanrad, Rolls-Royce Group plc, Blankenfelde-Mahlow, Germany; J. Tong, University of Portsmouth, Portsmouth, United Kingdom
Mr. David W. Trop Chief Engineer - Structures, Product Development and Technology Boeing Commercial Airplanes, Seattle, WA
Award Lunceon
1130 hrs AIAA-2012-1734 Fatigue crack growth in laser shock peened Ti-6AL-4V aerofoils subjected to foreign object damage
Wind Turbine Dynamics, Loads, and Control
A. Arcari, N. Apetre, S. Sarkar, N. Iyyer, B. Van Hooreweder, R. Boonen, D. Moens, Technical Data Analysis, Inc., Falls Church, J. Kruth, P. Sas, Catholic Univerity of VA; N. Dowling, Virginia Polytechnic Leuven, Heverlee, Belgium Institute and State University, Blacksburg, VA; S. Stanzl-Tschegg, University of Natural Resources and Life Sciences, Vienna, Austria; N. Phan, P. Kang, Naval Air Systems Command, Patuxent River, MD
1100 hrs AIAA-2012-1733 On the Determination of Fatigue Properties of Ti6Al4V Produced by Selective Laser Melting
Chaired by: R. NAIK, Pratt & Whitney and W. YU 0930 hrs 1000 hrs AIAA-2012-1730 AIAA-2012-1731 Statistical Analysis of Viscoelastic Creep Experimental investigation and model analysis of uncertain loading Compliance of Vinyl Ester Resin J. Simsiriwong, R. Sullivan, Mississippi State effect on fatigue crack growth 1030 hrs AIAA-2012-1732 Influence of superimposed VHCF loadings in cyclic fatigue of 7075-T6 aluminum alloy
Fatigue and Creep in Materials
Wednesday, 25 April 2012 86-SDM-59
Maui
Kahuku
Kohala
37
Boulder, Boulder, CO; K. Wilkie, NASA Langley Research Center, Hampton, VA; D. Lawrence, University of Colorado, Boulder, Boulder, CO
M. Lee, J. Ceisel, D. Mavris, Georgia Institute of Technology, Atlanta, GA
University, Dayton, OH
Chaired by: D. CHEN, The Boeing Company and R. KAPANIA 1500 hrs 1430 hrs AIAA-2012-1751 AIAA-2012-1750 A Parametric, High Fidelity Stiffening of Thermally Restrained Structural Analysis and Structures via Thermoelastic Optimization Tool with Topology Optimization Manufacturing Cost Considerations J. Deaton, R. Grandhi, Wright State
Wednesday, 25 April 2012 91-MDO-11
Surrey, Guildford, United Kingdom; A. Daton-Lovett, RolaTube Technology, Ltd., Lymington, United Kingdom Y. Shirasawa, O. Mori, H. Sawada, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; Y. Chishiki, K. Kitamura, University of Tokyo, Tokyo, Japan; J. Kawaguchi, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan
A. Baldomir, S. Hernandez, L. Romera, J. Diaz, University of Coruna, A Coruna, Spain
1530 hrs AIAA-2012-1752 Size Optimization of Shell Structures Considering Several Incomplete Configurations
S. Padula, J. Robinson, NASA Langley Research Center, Hampton, VA
1600 hrs AIAA-2012-1753 Structural Analysis in a Conceptual Design Framework
Structural Optimization
J. Kawaguchi, O. Mori, H. Sawada, R. Funase, Y. Tsuda, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan
1600 hrs AIAA-2012-1748 IKAROS, a Solar Sail Demonstrator and Its Application to Trojan Asteroid Exploration
Solar Sails
1600 hrs AIAA-2012-1742 Dynamic Response Tailoring for Efficient Morphing Control of Bistable Structures
Analysis and Design
J. Wittmann, M. Pleissner, A. Isikveren, M. Hornung, Bauhaus Luftfahrt e.V., Munich, A. Arrieta, P. Hagedorn, Technical Germany; M. Friswell, R. Ajaj, Swansea University of Darmstadt, Darmstadt, University, Swansea, United Kingdom; H. Germany Baier, Technical University of Munich, Munich, Germany
1530 hrs AIAA-2012-1741 Hierarchical Approach for Conceptual Design of Morphing Devices
Chaired by: D. MURPHY, ATK and G. GRESCHIK, TentGuild Engineering Company 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1745 AIAA-2012-1746 AIAA-2012-1747 The Completely Stripped Solar Sail Heliogyro Blade Twist Control via A Study on Membrane Deformation Concept Reflectivity Modulation of Solar Power Sail Demonstrator J. Fernandez, V. Lappas, University of D. Guerrant, University of Colorado, “IKAROS”
Wednesday, 25 April 2012 90-GSF-4
R. Ajaj, M. Friswell, Swansea University, University, Uxbridge, United Kingdom Swansea, United Kingdom; G. Allegri, University of Bristol, Bristol, United Kingdom; W. Dettmer, Swansea University, Swansea, United Kingdom; A. Isikveren, Bauhaus Luftfahrt e.V., Munich, Germany
Chaired by: R. BOTEZ, École de Technologie Superieure 1430 hrs 1500 hrs AIAA-2012-1739 AIAA-2012-1740 Optimization of a Corrugated Skin Optimum Design of a PID Controller for the Adaptive Torsion for a Morphable Winglet N. Ursache, C. Bell, C. Mares, Brunel Wing Using GA
Wednesday, 25 April 2012 89-ASC-5
S. Mulani, V. Duggirala, R. Kapania, Virginia Polytechnic Institute and State University, Blacksburg, VA
1630 hrs AIAA-2012-1754 Curvilinearly T-Stiffened Panel Optimization Framework under Multiple Load Cases Using Parallel Processing
H. Sawada, O. Mori, S. Matunaga, Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan; K. Kitamura, University of Tokyo, Tokyo, Japan; Y. Shirasawa, Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan; Y. Chishiki, University of Tokyo, Tokyo, Japan; T. Nishihara, Tokyo Institute of Technology, Tokyo, Japan
1630 hrs AIAA-2012-1749 Shape Estimation of IKAROS’s Solar Power Sail by Images of Monitor Cameras
S. Bradford, C. Ohara, F. Shi, G. Agnes, S. Hoffman, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; K. Wilkie, NASA Langley Research Center, Hampton, VA
1630 hrs AIAA-2012-1743 Piezocomposite Actuator Arrays for Correcting and Controlling Wavefront Error in Reflectors
M. Shimoda, Toyota Technological Institute, Nagoya, Japan
1700 hrs AIAA-2012-1755 Multi-objective Free-form Optimization of Shell Structures
W. Reynolds, D. Doyle, B. Arritt, Air Force Research Laboratory, Kirtland AFB, NM
1700 hrs AIAA-2012-1744 Active Health Monitoring of Complex Satellite Structures
Niihau
Honolulu
Kauai
38
J. Brezillon, A. Ronzheimer, D. Haar, M. Abu-Zurayk, M. Lummer, F. Natterer, German Aerospace Center (DLR), Braunschweig, Germany
Ann Arbor, Ann Arbor, MI
Pipes, Purdue University, West Lafayette, IN
University of Dresden, Dresden, Germany; CA; I. Cozmuta, NASA Ames Research E. Johann, Rolls-Royce Group plc, Center, Moffett Field, CA; J. Alonso, Blankenfelde-Mahlow, Germany Stanford University, Stanford, CA
Urbana-Champaign, Urbana, IL; A. Velicki, The Boeing Company, Huntington Beach, CA
1600 hrs AIAA-2012-1768 Design and Maintainability Considerations Regarding the Effects of Suborbital Flights on Composite Constructed Vehicles
Composites Structures
W. Kim, J. Lee, J. Hong, K. Kim, J. Choi, J. Kim, H. Sung, Korea Aerospace University, Goyang, South Korea
1630 hrs AIAA-2012-1769 Non-linear Modeling of ExtensionTwist Coupled Energy Absorbing Composite Tubes
1600 hrs AIAA-2012-1764 Reliability Analysis of Solid Rocket Motor under Bayesian Framework
1700 hrs AIAA-2012-1770 Sizing and Lifecycle Cost Analysis of an Ares V Composite Interstage
T. Mann, S. Smeltzer, B. Mason, R. C. Tiwari, E. Smith, C. Bakis, Pennsylvania Grenoble, NASA Langley Research Center, Hampton, VA; S. Rosario, Analytical R. Biggs, R. Cochran, Lockheed Martin E. Lundgren, The Aerospace Corporation, El State University, University Park, PA Mechanics Associates, Hampton, VA; B. Corporation, New Orleans, LA; B. Clark, Segundo, CA; J. Hanson, Federal Aviation Fairbairn, Vigyan, Hampton, VA Lockheed Martin Corporation, Fort Worth, TX; Administration, Washington, DC E. Pendleton, Air Force Research Laboratory, Wright-Patterson AFB, OH; K. Griffin, Southwest Research Institute, San Antonio, TX
Chaired by: K. LIN, University of Washington and J. RIMOLI, Georgia Institute of Technology 1500 hrs 1530 hrs 1430 hrs AIAA-2012-1766 AIAA-2012-1767 AIAA-2012-1765 Optimum Stress and Material On Compressive Response of Integrated Composite Structures Distributions in Stitched PRSEUS IM7/8552 Lamina- A Theoretical & Demonstration for Future Composites Experimental Review Space Launch Vehicle Airframe D. Lee, H. Hilton, University of Illinois, A. Hussien, M. Moehring, C. Schwall, B. Applications
Wednesday, 25 April 2012 94-SDM-61
M. Riley, University of Idaho, Moscow, Moscow, ID; R. Grandhi, Wright State University, Dayton, OH
1630 hrs AIAA-2012-1760 Economics of Laminar Aircraft Considering Off-Design Performance
E. Boekeloo, University of Michigan, Ann K. Franz, T. Lammering, K. Risse, E. Arbor, Ann Arbor, MI; A. Favaloro, Mississippi Anton, R. Hoernschemeyer, RWTH Aachen State University, Mississippi State, MS; T. University, Aachen, Germany Harris, Purdue University, West Lafayette, IN; L. Humphrey, Montana State University, Bozeman, MT; B. Johnson, Stanford University, Stanford, CA; T. Lake, Wichita State University, Wichita, KS; C. Mcatee, Auburn University, Auburn, AL; K. Scheider, Old Dominion University, Norfolk, VA; Y. Shimizu, Massachusetts Institute of Technology, Cambridge, MA; B. Tirey, University of Kentucky, Lexington, Lexington, KY
1600 hrs AIAA-2012-1759 Integrated Systems Design of a Cargo Aircraft with Environmentally Responsible Goals
Aircraft Optimization
Non-Deterministic Approaches for Aerospace Systems I
Chaired by: T. TORNG, The Boeing Company and S. MAHADEVAN, Vanderbilt University 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1761 AIAA-2012-1762 AIAA-2012-1763 A Novel Surrogate Modeling Principal component analysis on A Statistics-Based Material Property Technique for Parametric 3D scanned compressor blades for Analysis to Support Ablation Uncertainty Quantification in probabilistic CFD simulation Simulation UQ Efforts A. Lange, M. Voigt, K. Vogeler, Technical S. Copeland, Stanford University, Stanford, Simulation-Based Design
Wednesday, 25 April 2012 93-NDA-10
of Technology, Delft, The Netherlands
Chaired by: M. STELMACK, Lockheed Martin Corporation and S. HERNANDEZ, La Coruna University 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1756 AIAA-2012-1757 AIAA-2012-1758 Development and application of Optimal Flying Wings: A Numerical A Conceptual Design and Optimization Study Optimization Method for Blended- multi-disciplinary optimization capabilities based on high-fidelity C. Mader, University of Toronto, Toronto, Wing-Body Aircraft Canada; J. Martins, University of Michigan, R. Vos, J. van Dommelen, Delft University methods
Wednesday, 25 April 2012 92-MDO-12
Waianae
Oahu
Hilo
39
Space Center, Houston, TX; E. Bruno, United Space Alliance, Houston, TX; P. Deloo, ESA, Noordwijk, The Netherlands
J. Rome, V. Goyal, P. Schubel, D. Patel, G. Steckel, The Aerospace Corporation, El Segundo, CA
University, Wichita, KS
University, Wichita, KS
W. Zongren, J. Yang, M. Yang, W. Zhang, Beihang University, Beijing, China
1630 hrs AIAA-2012-1775 Experimental Investigation of Thermal Contact Conductance Between Titanium TC4 and Alloy Steel 30CrMnSi
1600 hrs AIAA-2012-1779 Elastic-Plastic Nonlinear Response of a Space Shuttle External Tank Stringer: Thermal and Mechanical Loadings
1630 hrs AIAA-2012-1780 STS-133/ET-137 Tanking Test Photogrammetry Assessment
L. Borkowski, M. Yekani Fard, A. Chattopadhyay, Arizona State University, Tempe, AZ
E. Swenson, T. Owens, Air Force Institute of Technology, Wright-Patterson AFB, OH
1600 hrs AIAA-2012-1786 Effects of Strain on the Propagation of PZT-induced Lamb Waves in Aluminum Plates Measured via 3D Laser Doppler Vibrometry
Health Monitoring
Y. Liu, A. Moncada, M. Yekani Fard, A. Chattopadhyay, Arizona State University, Tempe, AZ; M. Seaver, Naval Research Laboratory, Washington, DC
1630 hrs AIAA-2012-1787 A Statistical Approach to Investigate Temperature Effects on Guided Wave Based Structural Health Monitoring
S. Oliver, NASA Marshall Space Flight N. Knight, General Dynamics Corporation, Center, Huntsville, AL Chantilly, VA; J. Warren, K. Elliott, NASA Chantilly, VA; K. Song, ATK, Hampton, VA; Langley Research Center, Hampton, VA; K. Elliott, I. Raju, J. Warren, NASA Langley K. Song, ATK, Hampton, VA; I. Raju, NASA Langley Research Center, Hampton, VA Research Center, Hampton, VA
Chaired by: D. COPE, Southwest Research Institue and G. HRINDA, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1783 AIAA-2012-1784 AIAA-2012-1785 Structural Health Diagnosis Using A Hybrid Inference Approach Modeling Lamb Wave Propagation Deep Belief Network Based State for Health Diagnostics with for Damage Detection in a Complex Classification Unexampled Faulty States Metallic Aerospace Structural P. Tamilselvan, P. Wang, Wichita State P. Tamilselvan, P. Wang, Wichita State Component
Wednesday, 25 April 2012 97-SDM-64
R. Wingate, NASA Marshall Space Flight Center, Huntsville, AL
J. Worotynska, G. Vio, University of Sydney, Sydney, Australia; M. Berci, University of Leeds, Leeds, United Kingdom
1600 hrs AIAA-2012-1774 Initial Investigation of Chordwise Flexible Flat Aerofoil
Test and Analysis
STS-133/ET-137 Intertank Stringer Cracks
Chaired by: D. PHILLIPS, NASA Marshall Space Flight Center and K. ELLIOTT, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1776 AIAA-2012-1777 AIAA-2012-1778 Stress Analysis and Testing at the STS-133 Space Shuttle External Elastic-Plastic Nonlinear Response Marshall Space Flight Center to Tank Intertank Stringer Crack of a Space Shuttle External Study Cause and Corrective Action Investigation Stress Analysis Tank Stringer: Stringer-Feet B. Steeve, NASA Marshall Space Flight of Space Shuttle External Tank Imperfections and Assembly Center, Huntsville, AL N. Knight, General Dynamics Corporation, Stringer Failures
Wednesday, 25 April 2012 96-SDM-63
Hampton, VA; O. Valverde, National Institute of Aerospace, Hampton, VA; C. Stanfield, W. Doggett, NASA Langley Research Center, Hampton, VA
Chaired by: M. DOMB, Bombardier, Inc. and C. RANKIN, Rhombus Consultants Group, Inc. 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1771 AIAA-2012-1772 AIAA-2012-1773 Predicting and Measuring the Accelerated Creep Testing of High Structural Verification of the International Space Station Strength Reduction of Sandwich Strength Aramid Webbing T. Jones, NASA Langley Research Center, J. Zipay, K. Bernstein, NASA Johnson Structures with Spliced Foam Cores
Wednesday, 25 April 2012 95-SDM-62
E. Velazquez, J. Kosmatka, University of California, San Diego, La Jolla, CA
1700 hrs AIAA-2012-1788 Acoustic Emission Structural Health Monitoring of Laminated Composite Aircraft Structures
J. Saxon, R. Wingate, G. Swanson, W. Ondocsin, T. Boles, NASA Marshall Space Flight Center, Huntsville, AL
1700 hrs AIAA-2012-1781 Stringer Bending Test Helps Diagnose and Prevent Cracks in the Space Shuttle’s External Tank
Waialua
D. Phillips, J. Saxon, R. Wingate, NASA Marshall Space Flight Center, Huntsville, AL
Lanai 1730 hrs AIAA-2012-1782 Test-Analysis Correlation of the Single Stringer Bending Tests for the Space Shuttle ET-137 Intertank Stringer Crack Investigation
Kona
40
and State University, Blacksburg, VA; R. Vasconcellos, University of São Paulo, São Carlos, Brazil; A. Nayfeh, M. Hajj, Virginia Polytechnic Institute and State University, Blacksburg, VA; O. Badran, Al-Balqa Applied University, Amman, Jordan
P. Bansal, The Boeing Company, Bangalore, India; D. Pitt, N. Gurtowski, The Boeing Company, Saint Louis, MO
1500 hrs AIAA-2012-1795 Effects of Variations in Structural Properties of a Generic Wing on Flutter Prediction
S. Morton, U.S. Air Force, Eglin AFB, FL; S. Gibbs IV, I. Wang, L. Bloomhardt, E. S. Lamberson, Chenega Federal Systems, Dowell, Duke University, Durham, NC Eglin AFB, FL; D. McDaniel, University of Alabama, Birmingham, Birmingham, AL
Chaired by: C. SPIEKERMANN, The Aerospace Corporation 1500 hrs 1430 hrs AIAA-2012-1801 AIAA-2012-1800 Static and Dynamic Aeroelastic Aeroelastic Behavior of NoiseSimulations Using Kestrel - A Reducing Membranes for Aircraft CREATE Aircraft Simulation Tool Lifting Surfaces Part I: Theory
Wednesday, 25 April 2012 100-SDM-67
L. Butt, M. Bhatia, R. Kapania, Virginia Polytechnic Institute and State University, Blacksburg, VA
Chaired by: W. LUBER, EADS 1430 hrs AIAA-2012-1794 Flutter Modeling and Suppression for a Strut-Braced Wing
Wednesday, 25 April 2012 99-SDM-66
J. Dhainaut, Embry-Riddle Aeronautical University, Daytona Beach, FL
I. Wang, S. Gibbs IV, L. Bloomhardt, E. Dowell, Duke University, Durham, NC
S. Kukreja, NASA Dryden Flight Research Center, Edwards, CA; G. Vio, University of Sydney, Sydney, Australia; T. Andrianne, N. Razak, G. Dimitriadis, University of Liège, Liège, Belgium
1630 hrs AIAA-2012-1798 A Cross-Validation Approach to Approximate Basis Function Selection of the Stall Flutter Response of a Rectangular Wing in a Wind Tunnel
C. Jung, K. D`souza, B. Epureanu, University of Michigan, Ann Arbor, Ann Arbor, MI
1630 hrs AIAA-2012-1793 Bilinear amplitude approximation for piecewise-linear oscillators
1630 hrs AIAA-2012-1804 Aeroelastic Behavior of NoiseReducing Membranes for Aircraft Lifting Surfaces Part II: C. Dribusch, University of Arizona, Tucson, Experiments
1600 hrs AIAA-2012-1803 Construction of Aeroelastic Stability Boundaries Using a Multi-Fidelity Approach
Aeroelasticity II
N. Razak, G. Dimitriadis, J. Rothkegel, University of Liège, Liège, Belgium
1600 hrs AIAA-2012-1797 Experiments on a Pitch-Plunge Wing Undergoing Limit Cycle Oscillation
M. Karpel, Technion--Israel Institute of Technology, Haifa, Israel; A. Shousterman, Y. Tucson, AZ Mindelis, Israeli Computational Fluid Dynamics Center (ISCFDC), Caesarea, Israel
1530 hrs AIAA-2012-1802 Rigid-Body Issues in FFT-Based Dynamic Loads Analysis with Aeroservoelastic Nonlinearities
M. Nikbay, P. Acar, Istanbul Technical University, Istanbul, Turkey
1530 hrs AIAA-2012-1796 Flutter Based Aeroelastic Optimization of an Aircraft Wing with Analytical Approach
Flutter II
N. Nguyen, NASA Ames Research Center, Moffett Field, CA; K. Trinh, Stinger Ghaffarian Technologies, Inc., Moffett Field, CA; D. Nguyen, University of California, Berkeley, Berkeley, CA
1600 hrs AIAA-2012-1792 Nonlinear Aeroelasticity of Flexible Wing Structure Coupled with Aircraft Flight Dynamics
Nonlinear Dynamics and Aeroelasticity I
Technology, Inc., Scottsdale, AZ; L. Demasi, San Diego State University, San Diego, CA
Chaired by: E. SWENSON, Air Force Research Institute and O. SHIRYAYEV, Petroleum Institute Abu Dhabi 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1789 AIAA-2012-1790 AIAA-2012-1791 Nonlinear Analysis and Identification Dynamic Nonlinear Aeroelastic Nonlinear Finite Element Modal of Limit Cycle Oscillations in an Analysis of the Joined Wing Formulation for Panel Flutter Configuration with Thermal Effects and Acoustic Aeroelastic System A. Abdelkefi, Virginia Polytechnic Institute S. Bhasin, P. Chen, Z. Wang, ZONA Excitation
Wednesday, 25 April 2012 98-SDM-65
H. Sepic Kriskovich, H. Eslami, J. Ladesic, J. Dhainaut, Embry-Riddle Aeronautical University, Daytona Beach, FL
1700 hrs AIAA-2012-1799 Effects of Elastic Foundations on Flutter of High Aspect Ratio Wings
R. Vasconcellos, University of São Paulo, São Carlos, Brazil; A. Abdelkefi, Virginia Polytechnic Institute and State University, Blacksburg, VA; F. Marques, University of São Paulo, São Carlos, Brazil; M. Hajj, Virginia Polytechnic Institute and State University, Blacksburg, VA
1700 hrs AIAA-2012-1980 Control Surface Freeplay Nonlinearity: Modeling and Experimental Validation
Akaka Falls
Molokai
Koko Crater
41
Takeda, J. Scanlan, A. Keane, University of Southampton, Southampton, United Kingdom
X. Ning, S. Pellegrino, California Institute of Technology, Pasadena, CA
B. Gockel, Air Force Research Laboratory, K. Lonkar, S. Roy, V. Janapati, F. Chang, Wright-Patterson AFB, OH; A. Tudor, Stanford University, Stanford, CA University of California, Los Angeles, Los Angeles, CA; M. Brandyberry, University of Illinois, Urbana-Champaign, Urbana, IL; R. Penmetsa, E. Tuegel, Air Force Research Laboratory, Wright-Patterson AFB, OH
and State University, Blacksburg, VA
V. Varshney, J. Lee, A. Roy, Air Force Research R. Mohan, E. Fefey, A. Kelkar, North Laboratory, Wright-Patterson AFB, OH; T. Carolina A&T State University, Greensboro, Michalak, State University of New York, NC Albany, NY; B. Farmer, Air Force Research Laboratory, Wright-Patterson AFB, OH
Chaired by: G. ODEGARD; E. GLAESSGEN, NASA Langley Research Center and J. KOO, University of Texas, Austin 1500 hrs 1530 hrs 1430 hrs AIAA-2012-1820 AIAA-2012-1821 AIAA-2012-1819 Multiscale Modeling Analysis of the How does CNT Functionalization Predictive Mechanical Properties Interface Effects on the Mechanical and Epoxy Curing affects the of EPON 862 (DGEBF) cross-linked Properties of CNT-Polyethylene Thermal Interface Conductance with Curing Agent W (DETDA) and Nanocomposites in CNT-Epoxy Composites? An SWCNT using MD Simulations Y. Li, G. Seidel, Virginia Polytechnic Institute atomistic modeling perspective Effect of Carbon Vacancy Defects
Wednesday, 25 April 2012 103-SDM-70
Wright-Patterson AFB, OH
Chaired by: E. GLAESSGEN, NASA Langley Research Center and D. STARGEL, Air Force Office of Scientific Research 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1812 AIAA-2012-1813 AIAA-2012-1814 The Airframe Digital Twin: Some Challenges with Structural Life A Model-assisted Integrated Challenges to Realization Forecasting Using Realistic Mission Diagnostics for Structural Health E. Tuegel, Air Force Research Laboratory, Profiles Monitoring
Wednesday, 25 April 2012 102-SDM-69
T. van der Laan, L. Hootsmans, Fokker Aerostructures, Papendrecht, The Netherlands
Chaired by: C. DAUWALTER, Milli Sensor Systems and Actuators, Inc. and J. CUTSHALL 1430 hrs 1500 hrs 1530 hrs AIAA-2012-1805 AIAA-2012-1806 AIAA-2012-1807 Architecting a Decision Environment Design of Lightweight Structural An interactive conceptual Components for Direct Digital development environment for wing for Complex Design Evaluation D. Gorissen, E. Quaranta, M. Ferraro, K. Manufacturing box like structures
Wednesday, 25 April 2012 101-SDM-68
1630 hrs AIAA-2012-1816 Probabilistic fatigue life prediction using Subset Simulation
1630 hrs AIAA-2012-1823 Multiscale model for polymer-based nanocomposites considering phase transition behavior
Y. Liu, Clarkson University, Potsdam, NY
J. Choi, S. Yang, S. Yu, M. Cho, Seoul S. Roy, University of Alabama, Tuscaloosa, National University, Seoul, South Korea Tuscaloosa, AL; A. Nair,
1600 hrs AIAA-2012-1822 Concurrently Coupled Multiscale Modeling of Nano-Particle Reinforced Polymers in the Nonlinear Regime
Nanostructured Materials IV
Research Laboratory, Wright-Patterson AFB, OH
Kohala
J. Yu, T. Lacy, H. Toghiani, C. Pittman, Mississippi State University, Mississippi State, MS
1700 hrs AIAA-2012-1824 Micromechanically Based Effective Thermal Conductivity Estimates for Polymer Nanocomposites
Waimea Canyon
1730 hrs AIAA-2012-1818 The Digital Twin Paradigm for Future NASA and U.S. Air Force Vehicles
Puna
E. Glaessgen, S. Smith, NASA Langley Research Center, Hampton, VA; D. Stargel, B. Smarslok, Air Force Research Air Force Office of Scientific Research, Laboratory, Wright-Patterson AFB, OH; Arlington, VA S. Mahadevan, Vanderbilt University, Nashville, TN; A. Culler, Air Force Research Laboratory, Wright-Patterson AFB, OH
C. Levandowski, H. Johannesson, A. Forslund, R. Söderberg, Chalmers University of Technology, Göteborg, Sweden
1700 hrs AIAA-2012-1810 Platform Strategies from a PLM Perspective - Theory and Practice H. Briggs, ATA Engineering, San Diego, CA for the Aerospace Industry
1630 hrs AIAA-2012-1809 A Comparison of Design and Analysis Processes
1700 hrs AIAA-2012-1817 Error Quantification and Confidence Assessment of H. Li, Nanjing University of Aeronautics Aerothermal Model Predictions for R. Penmetsa, B. Gockel, R. John, Air Force and Astronautics, Nanjing, China; Y. Xiang, Hypersonic Aircraft
1600 hrs AIAA-2012-1815 Sensitivity Analysis of Structural Life Prediction Models in a Multiaxial Fatigue Environment
The Digital Twin Concept
S. Ghoman, Virginia Polytechnic Institute and State University, Blacksburg, VA; Z. Wang, P. Chen, ZONA Technology, Inc., Scottsdale, AZ; R. Kapania, Virginia Polytechnic Institute and State University, Blacksburg, VA
1600 hrs AIAA-2012-1808 A POD-based Reduced Order Design Scheme for Shape Optimization of Air Vehicles
Design Process
42
B. Jung, C. Cho, H. Yoon, H. Yoon, B. Youn, Y. Kim, Seoul National University, Seoul, South Korea
1530 hrs AIAA-2012-1828 Extension of MSC Nastran UVLM. OpenFSI for Rotational Applications Including Wind Turbines
1600 hrs AIAA-2012-1829 A Simplified Approach for Implicitly Considering Aerodynamics in the Seismic Response of Utility Scale Wind Turbines
Wind Turbine Aeroelasticity
Paquette, Sandia National Laboratories, Albuquerque, NM
Beltsville, MD; A. Flatau, J. Yoo, University A. Hadadian, R. Sedaghati, Concordia of Maryland, College Park, College University, Montréal, Canada; E. Esmailzadeh, Park, MD University of Ontario, Oshawa, Canada
1030 hrs AIAA-2012-1835 Optimal Design of Magnetorheological Damper using Response Surface Method
Systems and System Designs
Professor Vaios Lappas University of Surrey Guildford, United Kingdom
GSF Keynote: Gossamer Systems for Satellite Deorbiting: The CUBESAIL and DEORBITSAIL Space Missions
Thursday
Adaptive Energy Absorption for Transportation Systems Using Magnetorheological Fluids Professor Norman Werely University of Maryland
A. Abdelkefi, A. Nayfeh, M. Hajj, Virginia Polytechnic Institute and State University, Blacksburg, VA
1630 hrs 1700 hrs AIAA-2012-1830 AIAA-2012-1831 Thunderstorm Risks to Wind Farms Power Enhancement of H. Nguyen, L. Manuel, University of Piezoelectric Energy Harvesters Texas, Austin, Austin, TX; M. Barone, J. from Aeroelastic Vibrations
ASME Adaptive Structures and Materials Systems Prize Lecture
D. Corson, Altair Engineering, Clifton Park, Z. Wang, P. Chen, D. Sarhaddi, ZONA NY; D. Griffith, T. Ashwill, Sandia National Technology, Inc., Scottsdale, AZ; A. Diner, M. Asareh, I. Prowell, Missouri University Laboratories, Albuquerque, NM; F. Shakib, MSC Software Corporation, Santa Ana, CA of Science and Technology, Rolla, MO Altair Engineering, Mountain View, CA
Chaired by: W. REYNOLDS, Air Force Research Laboratory 0930 hrs 1000 hrs AIAA-2012-1834 AIAA-2012-1833 Development of Galfenol Based Statistical Model Calibration for Energy Harvesting Skin Analysis Non-Contact Torque Sensor A. Purekar, Techno-Sciences, Inc., and Design
Thursday, 26 April 2012 107-ASC-6
Thursday, 26 April 2012 106-GSF-5 0800 - 0900 hrs
Wednesday, 25 April 2012 105-ASME-1 1800 - 1900 hrs
K. Kecskemety, J. McNamara, Ohio State University, Columbus, OH
Chaired by: J. MCNAMARA, Ohio State University and D. GRIFFITH 1430 hrs 1500 hrs AIAA-2012-1826 AIAA-2012-1827 Investigating Aeroelastic Validation of an Enhanced Aeroelastic Analysis Code for Wind Performance of Multi-Mega Watt Wind Turbine Rotors Using CFD Turbines
Wednesday, 25 April 2012 104-SDM-71
Y. Yang, T. Strganac, Texas A&M University, College Station, TX
Kona
Kauai
Kauai
1730 hrs AIAA-2012-1832 Experiments of Vortex-Induced Vibration of a Flat Plate Exposed to a Normal Cross Flow
Kahuku
43
H. Sakamoto, Tokyo Institute of Technology, Tokyo, Japan; N. Kogiso, Osaka Prefecture University, Osaka, Japan; M. Okuma, Tokyo Institute of Technology, Tokyo, Japan
NeXolve Corporation, Huntsville, AL; J. Lin, ILC Dover, Frederica, DE; J. Moore, NeXolve Corporation, Huntsville, AL; H. Fang, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA
P. Rohl, P. Dorman, M. Sutton, Advatech Z. Zhu, M. van Tooren, Delft University of Pacific, San Bernardino, CA; C. Cesnik, D. Technology, Delft, The Netherlands Kumar, University of Michigan, Ann Arbor, Ann Arbor, MI
Hampton, VA; S. Kenny, D. Giesy, NASA Langley Research Center, Hampton, VA
L. Ng, Massachusetts Institute of Technology, Cambridge, MA; M. Eldred, Sandia National Laboratories, Albuquerque, NM
Chaired by: L. LURATI, The Boeing Company and J. WITTEVEEN 1000 hrs 0930 hrs AIAA-2012-1852 AIAA-2012-1851 Multifidelity Uncertainty Uncertainty Quantification for Polynomial Systems via Bernstein Quantification Using Non-Intrusive Polynomial Chaos and Stochastic Expansions L. Crespo, National Institute of Aerospace, Collocation
Thursday, 26 April 2012 111-NDA-11
A. Najafi, M. Rais-Rohani, Mississippi State S. DorMohammadi, M. Rais-Rohani, University, Mississippi State, MS Mississippi State University, Mississippi State, MS
1130 hrs AIAA-2012-1845 Study on disk and blade design based on multi-layer optimization strategy
H. Shi, B. Yang, University of Southern California, Los Angeles, CA; M. Thomson, H. Fang, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA
Young University, Provo, UT
S. DorMohammadi, M. Rais-Rohani, Mississippi State University, Mississippi State, MS
F. Viana, R. Haftka, University of Florida, Gainesville, Gainesville, FL; L. Watson, Virginia Polytechnic Institute and State University, Blacksburg, VA
1030 hrs AIAA-2012-1853 Probability of Failure Uncertainty Quantification with Kriging
M. Riley, University of Idaho, Moscow, ID; R. Grandhi, Wright State University, Dayton, OH
1100 hrs AIAA-2012-1854 Quantification of Modeling-Induced Uncertainties in Simulation-Based Design
Development of Non-Deterministic Methods II
S. Curtis, C. Mattson, B. Hancock, P. Lewis, Brigham Young University, Provo, UT
1130 hrs AIAA-2012-1850 An Empirical Accuracy and Computational Cost Study of Different P. Lewis, M. Tackett, C. Mattson, Brigham Methods in Analytical Target Cascading
1100 hrs AIAA-2012-1849 Considering Dynamic s-Pareto Frontiers in Decision Making
1130 hrs AIAA-2012-1840 Automatic Surface Mesh Generation for Design of Space Deployable Mesh Reflectors
S. Lee, S. Jun, S. Choi, Seoul National R. Wang, Z. Jia, J. Yang, Beihang University, Seoul, South Korea; Y. Kang, S. University, Beijing, China Yang, Korea Aerospace Research Institute, Daejeon, South Korea; D. Lee, Seoul National University, Seoul, South Korea
1100 hrs AIAA-2012-1844 Multidisciplinary Design Optimization of Axial Compressor with Double Step Optimization
Aircraft/Engine Optimization
O. Soykasap, S. Karakaya, Afyon Kocatepe University, Afyonkarahisar, Turkey
1100 hrs AIAA-2012-1839 Design and Testing of Ultra-Thin Shell Reflector Demonstrator
Deployable Apertures - RF
Multi-Objective and Multi-Level Optimization Methods
Chaired by: N. ALEXANDROV, NASA Langley Research Center and D. ALLAIRE, Massachusetts Institute of Technology 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1847 AIAA-2012-1848 AIAA-2012-1846 Reliability-Based Design Divergent Exploration in Design Multilevel Decomposition and Optimization of Coupled Process- Optimization Within Analytical with a Dynamic Multiobjective Performance Systems Target Cascading Framework Optimization Formulation
Thursday, 26 April 2012 110-MDO-14
A. Ronzheimer, M. Hepperle, J. Brezillon, O. Brodersen, German Aerospace Center (DLR), Braunschweig, Germany; J. Lieser, Rolls-Royce Group plc, BlankenfeldeMahlow, Germany
Chaired by: J. LEE, The Boeing Company and G. SINGH, General Electric Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1841 AIAA-2012-1842 AIAA-2012-1843 Aerodynamic Optimal Engine A Multidisciplinary Design A KBE Application for Automatic Integration for a Business Jet Environment for Composite Rotor Wire Harness Routing of Aircraft Configuration Blades Design
Thursday, 26 April 2012 109-MDO-13
Institute of Technology, Pasadena, CA; J. Costantine, California State University, Fullerton, CA; J. Banik, Air Force Research Laboratory, Kirtland AFB, NM
Chaired by: J. BANIK, U.S. Air Force and D. LICHODZIEJEWSKI, Airborne Systems North America 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1836 AIAA-2012-1837 AIAA-2012-1838 Finite-Element Model Updating for A Large and High Radio Frequency Structural Architectures for a Deployable Wideband UHF Antenna Highly Precise Tension-Stabilized Deployable Reflector G. Olson, S. Pellegrino, California L. Shook, ILC Dover, Frederica, DE; J. Pearson, Space Reflectors
Thursday, 26 April 2012 108-GSF-6
Kahuku
Niihau
Hilo
Honolulu
44
R. Dwight, H. Bijl, Delft University of Technology, Delft, The Netherlands; S. Timme, University of Liverpool, Liverpool, United Kingdom
Research Center, Hampton, VA; R. Pickell, The Boeing Company, Huntington Beach, CA
Technology, Gumi, South Korea
M. Hilburger, A. Lovejoy, NASA Langley Research Center, Hampton, VA; R. Thornburgh, Army Research Laboratory, Hampton, VA; C. Rankin, Rhombus Consultants Group, Palo Alto, CA
E. Cosentino, P. Weaver, University of Bristol, Bristol, United Kingdom
Institute of Science, Bangalore, India
Chaired by: C. BISAGNI, Technical University of Milan and C. BELDICA, University of Illinois 1000 hrs 1030 hrs 0930 hrs AIAA-2012-1870 AIAA-2012-1871 AIAA-2012-1869 On the Saint-Venant’s Principle Analytical Solutions for Dynamic On the Effect of Transverse and Asymptotic Expansions for Behavior of Pretwisted Anisotropic Normal Stresses in Shear-based Strip-like Beams Enhanced Single-layer Variational Anisotropic Beams and Plates A. Harish, D. Harursampath, Indian Formulations for Orthotropic Beams J. Kim, Kumoh National Institute of
Thursday, 26 April 2012 115-SDM-74
B. Kriegesmann, Leibniz University of Hannover, Hannover, Germany; M. Hilburger, NASA Langley Research Center, Hampton, VA; R. Rolfes, Leibniz University of Hannover, Hannover, Germany
Z. Kier, J. Rome, V. Goyal, P. Schubel, G. Steckel, D. Patel, Y. Kim, The Aerospace Corporation, El Segundo, CA; A. Waas, University of Michigan, Ann Arbor, Ann Arbor, MI
1100 hrs AIAA-2012-1863 Modeling Failure of 3D Fiber Reinforced Foam Core Sandwich Structures with Defects
Failure Analysis and Prediction II
T. Torng, The Boeing Company, Huntington T. Matsumura, R. Haftka, N. Kim, University of Beach, CA Florida, Gainesville, Gainesville, FL
1130 hrs AIAA-2012-1859 Discovering Multi-level Unexpected Failure Modes in Airplane Components Through Building-Block Tests
A. Harish, D. Harursampath, Indian Institute of Science, Bangalore, India
1100 hrs AIAA-2012-1872 Analytical Solutions for Dynamic Behavior of Thin-Walled OpenSection Composite Beams
Beam Analysis
1130 hrs AIAA-2012-1866 Preliminary Sizing Study of Ares-I and Ares-V Liquid Hydrogen Tanks
S. Oliver, NASA Marshall Space Flight L. Oremont, Lockheed Martin Corporation, Center, Huntsville, AL; D. Harper, The Hampton, VA; M. Schultz, NASA Langley Boeing Company, Huntsville, AL Research Center, Hampton, VA
1100 hrs AIAA-2012-1867 An Efficient Analysis Methodology for Fluted-Core Composite Structures
Developing the Next Generation of Shell Buckling Design Factors and Technologies II - Analysis and Design Technology
K. Karayev, P. Minguet, S. Lee, V. Balabanov, N. Muraliraj, The Boeing Company, Everett, WA; T. Walker, NSE Composites, Seattle, WA; E. Nelson, D. Robbins, D. Kenik, Firehole Composites, Laramie, WY
1030 hrs AIAA-2012-1862 Residual strength evaluation of typical aircraft composite structures with a large notch
University of Texas, San Antonio, San Antonio, TX
Chaired by: M. HILBURGER, NASA Langley Research Center and M. SCHULTZ, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1864 AIAA-2012-1865 AIAA-2012-1868 The Effects of Geometric and Loading Design and Analysis of Subscale Evaluation of Analysis Techniques Imperfections on the Response and and Full-Scale Buckling-Critical for Fluted-Core Sandwich Cylinders A. Lovejoy, M. Schultz, NASA Langley Lower-Bound Buckling Load of a Cylinders for Launch Vehicle Research Center, Hampton, VA Compression-Loaded Cylindrical Shell Technology Development
Thursday, 26 April 2012 114-SDM-73
M. Gunel, Turkish Aerospace Industries, Ankara, Turkey; A. Kayran, Middle East Technical University, Ankara, Turkey
Chaired by: J. WANG and M. SENSMEIER 0930 hrs 1000 hrs AIAA-2012-1860 AIAA-2012-1861 Linear and Non-linear Progressive Structural Integrity Testing Method Failure Analysis of Composite for PRSEUS Rod-Wrap Stringer Aerospace Structures Under Design J. Wang, R. Grenoble, NASA Langley Combined Loading
Thursday, 26 April 2012 113-SDM-72
L. Domyancic, Southwest Research Institute, San Antonio, TX; H. Millwater, University of Texas, San Antonio, San Antonio, TX
1100 hrs AIAA-2012-1858 Equivalent Initial Flaw Size Distribution Impact on Aircraft Risk Assessment
Non-Deterministic Approaches for Aerospace Systems II
Chaired by: R. GRAVES, Air Force Reseach Laboratory and R. GRANDHI, Wright State University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1855 AIAA-2012-1856 AIAA-2012-1857 Reducing Uncertainties in a Wind- Sensitivity Analysis for General Sensitivity Analysis for Risk Tunnel Experiment using Bayesian Aviation Risk Assessment Assessment of an Aircraft Fatigue M. Cortina, J. Ocampo, H. Millwater, Updating Critical Location
Thursday, 26 April 2012 112-NDA-12
Waimea Canyon
Lanai
Waianae
Oahu
45
Petroleum Institute, Abu Dhabi, United Arab Emirates
University, Morgantown, WV
O. Soto, J. Baum, SAIC, McLean, VA; R. Lohner, George Mason University, Fairfax, VA
J. Hobeck, D. Inman, University of Michigan, Ann Arbor, Ann Arbor, MI
Chaired by: B. WILLIS, The Boeing Company 1000 hrs 0930 hrs AIAA-2012-1882 AIAA-2012-1881 Photogrammetric Technique for Design and Analysis of Dual Pressure Probes for Predicting Center of Gravity Determination T. Jones, T. Johnson, NASA Langley Turbulence-Induced Vibration in Research Center, Hampton, VA Low Velocity Flow
Thursday, 26 April 2012 118-SDM-77
London, London, United Kingdom; P. Curtis, D. Pope, Defence Science and Technology Laboratory, Porton Down, United Kingdom
1100 hrs AIAA-2012-1880 Performance Evaluation of Shear Mode and Flow Mode Magnetorheological (MR) Energy Absorbers for Adaptive Seat Suspension Systems
Impact Dynamics
A. Dixit, D. Hodges, Georgia Institute of Technology, Atlanta, GA
1100 hrs AIAA-2012-1876 On static stability of damaged columns
Beam Dynamics II
K. Park, University of Colorado, Boulder, Boulder, CO; J. Kim, P. Lee, Korea Advanced Institute of Science and Technology, Daejeon, South Korea
1030 hrs AIAA-2012-1883 A Mode Selection Criterion Based on Flexibility Approach in Component Mode Synthesis
C. Foerster, University of California, San Diego, San Diego, CA; A. Valdes, Northrop Grumman Corporation, Rancho Bernardo, CA; J. Kosmatka, University of California, San Diego, San Diego, CA
1100 hrs AIAA-2012-1884 An Improved Ground Vibration Testing Approach of Flight Vehicle Structures Using a Scanning Laser Vibrometer
Experimental Dynamics Techniques
H. Singh, N. Wereley, University of Maryland, College Park, College Park, MD W. Hu, University of Maryland, College Park, College Park, MD; G. Hiemenz, G. Ngatu, Techno-Sciences, Inc., Beltsville, MD; N. Wereley, University of Maryland, College Park, College Park, MD
Chaired by: A. CULLER, Air Force Reseach Laboratory and Y. MATSUZAKI, Nagoya University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1877 AIAA-2012-1878 AIAA-2012-1879 Investigation of Factors Influencing An Efficient Coupled Fluid/ Influence of Occupant Compliance Dynamic Response of a Tensile Split Structure Finite Element Scheme on Optimal Control Performance Hopkinson Pressure Bar for Blast and Impact Loads over of a Vertically Stroking Seat T. Cwik, L. Iannucci, Imperial College Reinforced Concrete Structures Suspension
Thursday, 26 April 2012 117-SDM-76
G. Lesieutre, Pennsylvania State University, University Park, PA
Chaired by: M. ALLEN, University of Wisconsin and J. SLATER, Wright State University 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1873 AIAA-2012-1874 AIAA-2012-1875 Fatigue Crack Modeling and Axially-Moving Composite Beams A Viscous “Geometric” Beam Analysis in Beams Using Higher-Order ShearDamping Model that Results in P. Cooley, J. Slater, Wright State Deformation Theory Weak Frequency Dependence of University, Dayton, OH; O. Shiryayev, N. Sivaneri, G. Nagappan, West Virginia Modal Damping
Thursday, 26 April 2012 116-SDM-75
Waialua
Akaka Falls
Molokai
46
B. Lenahen, A. Bernier, S. Gangadharan, Embry-Riddle Aeronautical University, Daytona Beach, FL
Horsham, PA; S. Clay, Air Force Research Laboratory, Wright-Patterson AFB, OH
Wales at the Australian Defence Force Academy, Canberra, Australia
Michigan, Ann Arbor, Ann Arbor, MI
M. Chen, Air Force Research Laboratory, Wright-Patterson AFB, OH; C. Tseng, Universal Technology Corporation, Dayton, OH; R. Sikorski, Air Force Research Laboratory, Wright-Patterson AFB, OH; R. Viskanta, Purdue University, West Lafayette, IN
1100 hrs AIAA-2012-1901 Foam Property and Its Role in the Radiative Heat Transfer of Hybrid Materials
Z. Tabatabaei, J. Volz, Missouri University Davis, Jet Propulsion Laboratory, California G. Lubineau, J. Yagoubi, Cohmas-Kaust, Institute of Technology, Pasadena, CA of Science and Technology, Rolla, MO Thuwal, Saudi Arabia; A. Askari, The Boeing Company, Seattle, WA
Aerospace Materials Applications
Chaired by: D. POWELL, Southern Research Institute and W. YU 1000 hrs 0930 hrs AIAA-2012-1899 AIAA-2012-1898 Amorphous Metals for Aerospace Behavior of Long Carbon Fiber Reinforced Concrete Panels under Applications G. Agnes, D. Hofmann, A. Shapiro, G. Impact Loading 1030 hrs AIAA-2012-1900 Cyclic hygrothermal aging of aircraft lightning protections: phenomenological overview
D. Liu, Z. Wan, C. Yang, Beihang University, Beijing, China
1130 hrs AIAA-2012-1897 Electric Current Analysis for Thick Laminated CFRP Composites
M. Mordasky, W. Chen, Purdue University, A. Todoroki, Tokyo Institute of Technology, West Lafayette, IN Tokyo, Japan
1100 hrs AIAA-2012-1896 Instrumented Projectile Impact on Composites
Thursday, 26 April 2012 122-SDM-81
A. Nogueira, K. Drechsler, Fraunhofer, Augsburg, Germany; E. Hombergsmeier, EADS, Munich, Germany
C. Cheung, K. Lin, P. Gray, University of Washington, Seattle, Seattle, WA
1130 hrs AIAA-2012-1994 The Influence of Spar Position on Aeroelastic Optimization of a Large Aircraft Wing with Different Materials
Characterization of Composite Materials
Chaired by: G. SEIDEL, Virginia Polytechnic Institute and State University and S. WANTHAL, The Boeing Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1893 AIAA-2012-1894 AIAA-2012-1895 Analysis of the Static and Fatigue Identification and Characterization The Interaction of Failure Modes Strength of a Damage Tolerant of Debonded and Weakly Bonded in the Compression Response and 3D-Reinforced Joining Technology Structures Failure of Laminated Composites R. Heslehurst, University of New South P. Prabhakar, A. Waas, University of on Composite Single Lap Joints
Thursday, 26 April 2012 121-SDM-80
R. Smith, W. Langford, NASA Langley Research Center, Hampton, VA
1100 hrs AIAA-2012-1892 Design and Optimization of an Axial Mode II Crack Arrest Specimen
Design, Composite Structures
1100 hrs AIAA-2012-1888 A CFD Study of Cryogenic LH2 Tank Ullage Pressurization
Dynamics of Fuel Slosh and Tanks
J. Schotte, ONERA, Châtillon, France; R. D. Leuva, S. Gangadharan, Embry-Riddle Ohayon, National Conservatory of Arts and Aeronautical University, Daytona Beach, FL Crafts (CNAM), Paris, France
1030 hrs AIAA-2012-1887 Effect of internal liquids on the vibrations of aerospace structures
Chaired by: S. ROWE, NASA Marshall Space Flight Center and J. SCHRELL, General Electric Company 0930 hrs 1000 hrs 1030 hrs AIAA-2012-1889 AIAA-2012-1890 AIAA-2012-1891 Design, Analysis and Fabrication of Improved Methodologies for Material Quality of Braided Secondary Structural Components Damage Tolerant Composite Fuselage Profiles K. Birkefeld, T. von Reden, K. Drechsler, for the Habitat Demonstration Unit Structure Qualification J. Schutte, Materials Sciences Corporation, University of Stuttgart, Stuttgart, Germany - Deep Space Habitat
Thursday, 26 April 2012 120-SDM-79
B. Lenahen, A. Bernier, G. Peters, S. Gangadharan, Embry-Riddle Aeronautical University, Daytona Beach, FL
Chaired by: T. KINNEY, NASA Kenndey Space Center 0930 hrs 1000 hrs AIAA-2012-1885 AIAA-2012-1886 A Computational Investigation A Comparison Investigation of Experimental and Computational for Determining the Natural Frequencies and Damping Effects Fuel Slosh Models Utilizing Diaphragm-Implemented of Diaphragm-Implemented Spacecraft Propellant Tanks Spacecraft Propellant Tanks
Thursday, 26 April 2012 119-SDM-78
Kauai
Kohala
Puna
Koko Crater
47
K. Lyle, L. Horta, NASA Langley Research Center, Hampton, VA
University, Cheongju, South Korea; C. Jenkins, Montana State University, Bozeman, MT
K. Kwok, S. Pellegrino, California Institute of Technology, Pasadena, CA
1400 hrs AIAA-2012-1910 Micromechanical modeling of deployment and shape recovery of thin-walled viscoelastic composite space structures
J. Bakalyar, C. Jutte, NASA Dryden Flight Research Center, Edwards, CA
1400 hrs AIAA-2012-1904 Validation Tests of Fiber Optic Strain-Based Operational Shape and Load Measurements
Wrinkling and Non-Linear Effects
M. Santer, A. Saturni, Imperial College London, London, United Kingdom
1430 hrs AIAA-2012-1911 Time-Dependent Behavior of Thin CFRP Flexures
Materials and Testing
S. Vasista, L. Tong, University of Sydney, Sydney, Australia
1430 hrs AIAA-2012-1905 Pressurized Morphing Wing Structures
Aerospace System Applications II
Q. Wang, Massachusetts Institute of Technology, Cambridge, MA
Chaired by: F. ENGELSEN 1300 hrs AIAA-2012-1921 Sensitivity computation of periodic and chaotic limit cycle oscillations
Thursday, 26 April 2012 126-MDO-15
R. Orszulik, J. Shan, York University, Toronto, Canada
1500 hrs AIAA-2012-1918 Local Buckling in Crease Induced by Wrapping Fold of Space Membrane
State University, Blacksburg, VA; D. Di Maio, N. Ameri, D. Ewins, University of Bristol, Bristol, United Kingdom
Institute and State University, Blacksburg, National Institute for Research in Computer Science and Control, Sophia-Antipolis, France VA
Toronto, Canada; J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI
P. Ciampa, B. Nagel, German Aerospace Center (DLR), Hamburg, Germany
1500 hrs AIAA-2012-1925 Aeroelastic Design and Optimization of Unconventional I. Ghazlane, G. Carrier, M. Marcelet, A. Aircraft Configurations in a G. Kenway, G. Kennedy, University of Toronto, D. Cross, R. Canfield, Virginia Polytechnic Dumont, ONERA, Meudon, France; J. Desideri, Distributed Design Environment
1400 hrs AIAA-2012-1923 Solving Continuum Shape Sensitivity with Existing Tools for Nonlinear Aeroelastic Gust Analysis
1430 hrs AIAA-2012-1924 Aerostructural Adjoint Method for Flexible Wing Optimization
Aerostructural and Aeroelastic Optimization
1330 hrs AIAA-2012-1922 A Scalable Parallel Approach for High-Fidelity Aerostructural Analysis and Optimization
G. Valle, NASA Johnson Space Center, Houston, TX
K. Senda, K. Nakanishi, Kyoto University, Kyoto, Japan
1530 hrs AIAA-2012-1919 Wrinkle Generation Mechanism without Buckling in Sheared Rectangular Membrane
1530 hrs AIAA-2012-1913 Utilizing Photogrammetry and Strain Gage Measurement to Characterize Pressurization of an P. Tarazaga, Virginia Polytechnic Institute and Inflatable Module
1500 hrs AIAA-2012-1912 Continuous Laser Scanning of a Lightweight Membrane with Monotone and Multi-tone Excitation Techniques
R. Barnhart, R. Barrett, University of Kansas, Lawrence, Lawrence, KS
1500 hrs AIAA-2012-1906 Piezoelectric Adaptive Flutter Test Vane: Low Net Passive Stiffness (LNPS) Techniques for Deflection Amplification
Y. Satou, H. Furuya, Tokyo Institute of H. Furuya, J. Yokoyama, Tokyo Institute of Technology, Yokohama, Japan Technology, Yokohama, Japan
Chaired by: J. SLATER, Wright State University and G. DAVIS, Jet Propulsion Laboratory, California Institute of Technology 1300 hrs 1330 hrs 1400 hrs 1430 hrs AIAA-2012-1914 AIAA-2012-1915 AIAA-2012-1916 AIAA-2012-1917 Finite Element Analysis of a Deployment Analysis of a Tearing of Thin Membranes: Tear Wrinkle and Collapsing Process of Wrinkled Rectangular Membrane Simple Tape-Spring Hinge Using Propagation Direction Inflatable Tubes Under Bending K. Woo, Y. Kim, Chungbuk National with Elliptical Boundary Cuts Probabilistic Methods Loads by Finite Element Analyses
Thursday, 26 April 2012 125-GSF-8
D. Bergman, B. Yang, University of Southern Institute of Technology, Pasadena, CA; J. California, Los Angeles, CA; G. Davis, H. Fang, Mejia-Ariza, L’Garde, Inc., Tustin, CA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA
Chaired by: C. JENKINS, Montana State University 1300 hrs 1330 hrs AIAA-2012-1907 AIAA-2012-1909 Modeling and Quasi-Static Analysis of Characterization of a high strain a Shape Memory Polymer Cantilever composite material I. Maqueda, S. Pellegrino, California Beam for Space Applications
Thursday, 26 April 2012 124-GSF-7
O. Bilgen, E. Saavedra Flores, M. Friswell, B. LaCroix, P. Ifju, University of Florida, Swansea University, Swansea, United Gainesville, Gainesville, FL Kingdom
Chaired by: R. BARRETT, Auburn University 1300 hrs 1330 hrs AIAA-2012-1902 AIAA-2012-1903 Finite Element Modeling of Macro Implementation of a Fiber Composite Piezoelectric Continuous-Inextensible-Surface Actuators on Micro Air Vehicles Piezocomposite Airfoil
Thursday, 26 April 2012 123-ASC-7
Maui
Hilo
Kona
Kauai
48
Simon Fraser University, Surrey, Canada
D. Villanueva, R. Haftka, B. Sankar, University of Florida, Gainesville, Gainesville, FL
K. Kang, C. Lim, Y. Kim, Korea Aerospace University, Goyang, South Korea; D. Lee, Dongeui University, Busan, South Korea; J. Choi, Korea Aerospace University, Goyang, South Korea
Arizona, Tucson, Tucson, AZ H. Hur, Agency for Defense Development (ADD), Yuseong, South Korea; J. Park, Korea Aerospace University, Koyang-shi, South Korea
A. Vanaerschot, Catholic Univerity of Leuven, Leuven, Belgium; M. Olave, Ikerlan Technological Research Center, Mondragon, Spain; S. Lomov, D. Vandepitte, Catholic Univerity of Leuven, Leuven, Belgium
L. Demasi, San Diego State University, San Diego, CA
Chaired by: R. KOCH, Naval Undersea Warfare Center and K. LIU, Arizona State University 1330 hrs 1400 hrs 1300 hrs AIAA-2012-1945 AIAA-2012-1946 AIAA-2012-1944 Partially Layerwise Advanced Zig- Micro-structural Modeling for 2-D Ordinary State-Based Peridynamic Zag and HSDT Models Based on the Strengthened Plain Woven Textile Material Constants E. Oterkus, E. Madenci, University of Generalized Unified Formulation Composites
Thursday, 26 April 2012 130-SDM-82
V. Babuska, Sandia National Laboratories, Albuquerque, NM; S. Lacy, Air Force Research Laboratory, Kirtland AFB, NM; T. Paez, MannaTech Engineering, Albuquerque, NM
D. Villanueva, R. Le Riche, G. Picard, École Nationale Supérieure des Mines de Saint-Étienne, Saint-Étienne, France; R. Haftka, University of Florida, Gainesville, Gainesville, FL
1430 hrs AIAA-2012-1935 Surrogate-Based Agents for Constrained Optimization A. Najafi, Mississippi State University, Starkville, MS; E. Acar, TOBB University of Economics and Technology, Ankara, Turkey; M. Rais-Rohani, Mississippi State University, Starkville, MS
S. Muder, E. Armanios, University of Texas, Arlington, Arlington, TX
1430 hrs AIAA-2012-1947 Optimal Stacking Sequences for Thermally Induced Twist Deformation
Composites Modeling
K. Liu, A. Chattopadhyay, Arizona State University, Tempe, AZ
1500 hrs AIAA-2012-1948 Strain Rate Dependent Multiscale Modeling of Woven Composites Including Material and Geometrical Nonlinearity
1500 hrs AIAA-2012-1943 Sensitivity Analysis of Extreme Pressure Loads to Inflow Disturbance Parameters
C. Dubinsky, G. Singh, H. Millwater, S. Ben Ayed, S. Ragab, M. Hajj, Virginia University of Texas, San Antonio, San Polytechnic Institute and State University, Antonio, TX; P. Golden, Air Force Research Blacksburg, VA Laboratory, Wright-Patterson AFB, OH
1430 hrs AIAA-2012-1942 Experimental Resource Allocation for Statistical Simulation of Fretting Fatigue Problem
L. Mainini, Massachusetts Institute of Technology, Cambridge, MA; P. Maggiore, Technical University of Turin, Turin Italy
1530 hrs AIAA-2012-1931 A Multifidelity Approach to Aerodynamic Analysis in an Integrated Design Environment
J. Dizy, R. Palacios, S. Pinho, Imperial College London, London, United Kingdom
1530 hrs AIAA-2012-1949 Homogenization of slender periodic composite structures
1500 hrs AIAA-2012-1936 Robust Design of Energy Absorbing Components Considering The Manufacturing Effects
Engineering Applications of Non-Deterministic Approaches II
1400 hrs AIAA-2012-1934 A Nested Extreme Response Surface Approach for RBDO with Time-Dependent Probabilistic Constraints Z. Wang, P. Wang, Wichita State University, Wichita, KS
J. Zhang, S. Chowdhury, Rensselaer A. Orr, T. Robinson, Queen’s University Polytechnic Institute, Troy, NY; A. Messac, Belfast, Belfast, United Kingdom Syracuse University, Syracuse, NY
1500 hrs AIAA-2012-1930 Discipline-Specific Trust-Region Sizes for Variable-Fidelity Multidisciplinary Optimization
Non-Deterministic Design and Optimization
of Southampton, Southampton, United Kingdom
Chaired by: B. BICHON, Southwest Research Institute and M. ENRIGHT, Southwest Research Institute 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1937 AIAA-2012-1938 AIAA-2012-1939 Modeling and Simulation of Non-deterministic Vibration Analysis A stochastic multi-scale framework Parameter Vector Random of Degraded Polymer Structure Under for textile composites to evaluate the Processes in Mechanical Structures Environmental Changes stiffness tensor
Thursday, 26 April 2012 129-NDA-14
M. Vasile, University of Strathclyde, Glasgow, United Kingdom; E. Minisci, University of Glasgow, Glasgow, United Kingdom; Q. Wijnands, ESA, Noordwijk, The Netherlands
Chaired by: D. MAVRIS, Georgia Institute of Technology 1300 hrs 1330 hrs AIAA-2012-1932 AIAA-2012-1933 Approximated Computation of Accounting for Future Redesign in Belief Functions for Robust Design the Optimization of an Integrated Optimization Thermal Protection System
Thursday, 26 April 2012 128-NDA-13
W. Yamazaki, Nagaoka University of Technology, Nagaoka, Japan
1430 hrs AIAA-2012-1929 Domain Segmentation based on Uncertainty in the Surrogate (DSUS)
Surrogate-based and Multi-fidelity Optimization Methods
Chaired by: V. TOROPOV, University of Leeds and B. STANFORD, Air Force Research Laboratory 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1926 AIAA-2012-1927 AIAA-2012-1928 Design Optimization on “whiteHandling Constraints in SurrogateEfficient Robust Design Optimization by Variable Fidelity box” Uncovered by Metamodeling Based Optimization Z. Pirmoradi, K. Haji Hajikolaei, G. Wang, J. Parr, A. Forrester, A. Keane, University Kriging Model
Thursday, 26 April 2012 127-MDO-16
Waianae
Oahu
Kahuku
Niihau
49
M. Embley, D. Jensen, Brigham Young University, Provo, UT; C. Garvin, Novatek, Provo, UT; M. Jensen, Altus Poles, Provo, UT
of Technology, Atlanta, GA
of Arizona, Tucson, Tucson, AZ
M. Yekani Fard, Y. Liu, A. Chattopadhyay, T. Ricks, T. Lacy, Mississippi State Arizona State University, Tempe, AZ University, Mississippi State, MS; B. Bednarcyk, S. Arnold, NASA Glenn Research Center, Cleveland, OH
Chaired by: M. MAHLER, Raytheon Company and R. TAYLOR, Optimal Structures, LLC 1330 hrs 1400 hrs 1300 hrs AIAA-2012-1964 AIAA-2012-1965 AIAA-2012-1963 Fully Coupled Peridynamic Analytical and Statistical A Multiscale Modeling Methodology Thermomechanics Approaches to Flexural Behavior for Metal Matrix Composites A. Agwai, I. Guven, E. Madenci, University for Epoxy Resin Materials Including Fiber Strength Stochastics
Thursday, 26 April 2012 133-SDM-85
Polytechnic Institute and State University, Blacksburg, VA
Chaired by: M. HYER, Virginia Polytechnic Institute and State University and J. ZIPAY, NASA Johnson Space Center 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1957 AIAA-2012-1958 AIAA-2012-1959 Buckling and Crack Propagation of Influence of Consolidating Sleeves Stability Analysis of Columns with Cracked Box Beams and Geometric Scale on Buckling Imperfection H. Lo, R. Kapania, M. Patil, Virginia Z. Sotoudeh, D. Hodges, Georgia Institute After Impact of Basalt Columns
Thursday, 26 April 2012 132-SDM-84
Wilt, Air Force Research Laboratory, Kirtland AFB, NM; J. Footdale, LoadPath, Albuquerque, NM
1430 hrs AIAA-2012-1953 Model Calibration Efforts for the International Space Station’s Solar Array Mast
Deployable Structures 1500 hrs AIAA-2012-1954 Dynamic Behavior of a Low Inertia Gravity Off-load Passive Device
A. Sathiskumar, D. Harursampath, Indian Institute of Science, Bangalore, India; A. Uthandi, Aeronautical Development Agency, Bangalore, India
1430 hrs AIAA-2012-1966 Nonlinear Modeling of Piezocomposite Actuators with Application to Flapping Wing Micro Aerial Vehicles
Modeling
G. Houston, D. Quinn, A. Murphy, Queen’s University Belfast, Belfast, United Kingdom; C. Glazebrook, F. Bron, Constellium CRV, Voreppe, France
1430 hrs AIAA-2012-1960 The Impact of Geometric Imperfections on Metallic Stiffened Panels with Skin Bay Buckling Containment Features
Buckling
J. Li, H. Wang, Shanghai Jiao Tong University, Shanghai, China; N. Kim, University of Florida, Gainesville, Gainesville, FL
1500 hrs AIAA-2012-1967 A new moving least square response surface method for structural reliability analysis
M. Quatmann, H. Reimerdes, RWTH Aachen University, Aachen, Germany
1500 hrs AIAA-2012-1961 Computationally efficient analysis of the postbuckling behaviour of stiffened fuselage sections
E. Ardelean, Schafer Corporation, Albuquerque, NM; B. Cooper, Air Force K. Elliott, J. Templeton, NASA Langley Chantilly, VA; K. Song, ATK, Hampton, VA; Research Center, Hampton, VA; N. Knight, Research Laboratory, Kirtland AFB, NM; S. W. Belvin, NASA Langley Research Center, Hampton, VA; M. Zander, German Aerospace K. Elliott, NASA Langley Research Center, General Dynamics Corporation, Chantilly, Jeon, CSA Engineering, Albuquerque, NM Hampton, VA; J. Rayburn, NASA Marshall VA; K. Song, ATK, Hampton, VA Center (DLR), Braunschweig, Germany; D. Sleight, J. Connell, N. Holloway, NASA Langley Space Flight Center, Huntsville, AL Research Center, Hampton, VA; F. Palmieri, National Institute for Aerospace, Hampton, VA
Chaired by: J. DOMBER, Ball Aerospace & Technologies Corporation and J. MIN, NASA Glenn Research Center 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1950 AIAA-2012-1951 AIAA-2012-1952 Materials, Structures and FAST Mast Single-Bay Structural Modular Reconfigurable Zero Manufacturing: An Integrated Response to Axial Loading: Free-Play (MORF) Solar Array Modeling and Verification Deployment Concept Verification Approach to Develop Expandable G. Thomas, J. Banik, T. Murphey, D. N. Knight, General Dynamics Corporation, Structures
Thursday, 26 April 2012 131-SDM-83
G. Singh, J. Ocampo, H. Millwater, University of Texas, San Antonio, San Antonio, TX
1530 hrs AIAA-2012-1968 Extreme Value Modeling and Parametric Investigations of Gust and Maneuver Loads for General Aviation
K. Masuda, D. Chen, Tokyo University of Science, Chiyoda-ku, Japan
Waimea Canyon
Honolulu
E. Picault, S. Bourgeois, B. Cochelin, National Center for Scientific Research (CNRS), Marseille, France; F. Guinot, Thales Alenia Space, Cannes La Bocca, France
1600 hrs AIAA-2012-1956 On the folding and deployment of tape springs: A large displacements and large rotations rod model with highly flexible thin-walled crosssections
1530 hrs AIAA-2012-1962 Study on Bending Collapse of Thin Plate with Corrugated Cross-Section
J. Fernandez, University of Surrey, Guildford, United Kingdom; J. Banik, Air Force Research Laboratory, Kirtland AFB, NM
1530 hrs AIAA-2012-1955 Creep Effects and Deployment Characterization of Rollable Composite Shell Reflectors
Lanai
50
Hampton, VA; A. Przekop,
C. de Souza, R. da Silva, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; C. Cesnik, University of Michigan, Ann Arbor, Ann Arbor, MI
C. Altenbuchner, J. Hubbard, National Institute of Aerospace, Hampton, VA
R. Towner, J. Band, Jacobs, Huntsville, AL Institute of Technology, Atlanta, GA
Chaired by: B. COYNE, United Launch Alliance and K. HALL, Duke University 1330 hrs 1300 hrs AIAA-2012-1989 AIAA-2012-1987 An Analysis Technique/Automated Model Updating in Structural Tool for Comparing and Tracking Dynamics through a Confluence Analysis Modes of Different Finite Approach M. Chierichetti, M. Ruzzene, Georgia Element Models
Thursday, 26 April 2012 137-SDM-89
Laboratory, Wright-Patterson AFB, OH
Chaired by: C. CESNIK, University of Michigan 1300 hrs 1330 hrs AIAA-2012-1981 AIAA-2012-1982 Proper Modes for Modeling A Flexible Multibody Structural Flapping Dynamics of Ornithopters Dynamics Model with Experimental J. Slater, Wright State University, Dayton, Validation for a Research OH; D. Doman, Air Force Research Ornithopter
Thursday, 26 April 2012 136-SDM-88
S. Durmaz, M. Kaya, Istanbul Technical University, Istanbul, Turkey
“La Sapienza”, Rome, Italy; P. Marzocca, Clarkson University, Potsdam, NY
K. Tamma, University of Minnesota, Minneapolis, Minneapolis, MN
1400 hrs AIAA-2012-1990 A New and Robust Order Preserving Computational Framework for Index 3 DAE Multibody Dynamics Systems: Two-Field Form
1400 hrs AIAA-2012-1983 Global and Local Optimization of Flapping Kinematics M. Ghommem, M. Hajj, L. Watson, Virginia Polytechnic Institute and State University, Blacksburg, VA
1500 hrs AIAA-2012-1973 Dynamic Simulation of Geometrically Nonlinear Membranes Using Hermite Time Interpolation
A. Matney, Arizona State University, Tempe, AZ; S. Spottswood, Air Force Research D. Kunz, K. Kolsti, Air Force Institute of Laboratory, Wright-Patterson AFB, OH; M. Technology, Wright-Patterson AFB, OH Mignolet, Arizona State University, Tempe, AZ
1430 hrs AIAA-2012-1972 Nonlinear Structural Reduced Order Modeling Methods for Hypersonic Structures
Nonlinear Dynamics
1530 hrs AIAA-2012-1986 Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
A. Cammarano, University of Bristol, Bristol, United Kingdom; A. Carrella, LMS International, Leuven, Belgium
1500 hrs AIAA-2012-1992 Numerical Simulation and Experimental Verification of the Electro-Impulse De-Icing System
1530 hrs AIAA-2012-1974 Dynamics of non-linear structures: modal interaction and non-linear identification
A. El Arras, C. Chung, Y. Na, S. Shin, Seoul J. Jacob, Oklahoma State University, National University, Seoul, South Korea Stillwater, OK; S. Smith, University of Kentucky, Lexington, Lexington, KY; L. Asheghian, NextGen Aeronautics, Torrance, CA; W. Loh, Oklahoma State University, Stillwater, OK
1500 hrs AIAA-2012-1985 Various Structural Approaches to Analyze an Aircraft with High Aspect Ratio Wings
K. Ni, Advanced Dynamics, Inc., Lexington, KY
1500 hrs AIAA-2012-1979 Flutter and LCO of a All-movable Horizontal Tail with Freeplay
A. Kundu, S. Adhikari, Swansea University, Q. Li, T. Bai, C. Zhu, Nanjing University of Swansea, United Kingdom Aeronautics and Astronautics, Nanjing, China
1430 hrs AIAA-2012-1991 Transient Dynamics of Stochastic Structural Systems using a Reduced Order Spectral Function Approach
Modeling and Simulation
U. Chakravarty, Air Force Research Laboratory, Eglin AFB, FL
1430 hrs AIAA-2012-1984 Natural Frequencies and Mode Shapes of the Wings of LowReynolds-Number Flyers
Dynamics of Micro-Aircraft
F. Sebastiano, G. Quaranta, S. Ricci, Technical University of Milan, Milan, Italy
1430 hrs AIAA-2012-1978 Experimental and numerical investigation of the behavior of a T-tail with control surface freeplay
Nonlinear Dynamics and Aeroelasticity II
Chaired by: K. NAGARAJA, The Boeing Company and M. ROSS, Sandia National Laboratories 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1975 AIAA-2012-1976 AIAA-2012-1977 Limit Cycle Oscillations of Swept- A Nonlinear Aeroelastic Frame Post-Flutter Analysis of Flexible back Wings In an Incompressible Based on UVLM and a Composite High-Aspect-Ratio Wings A. Arena, W. Lacarbonara, University of Rome Flow Corotational Shell Fe
Thursday, 26 April 2012 135-SDM-87
K. Carlberg, J. Cortial, C. Farhat, Stanford Sracic, University of Wisconsin, Madison, Madison, WI University, Stanford, CA
Chaired by: S. RIZZI, NASA Langley Research Center and A. SCOTTI, Pilatus Aircraft, Ltd. 1300 hrs 1330 hrs 1400 hrs AIAA-2012-1969 AIAA-2012-1970 AIAA-2012-1971 Efficient structure-preserving model A Numerical Continuation Method Nonlinear Reduced-Order Simulation Using an Experimentally reduction for nonlinear mechanical to Compute Nonlinear Normal Modes Using Modal Reduction Guided Modal Basis systems with application to M. Allen, R. Kuether, B. Deaner, M. S. Rizzi, NASA Langley Research Center, structural dynamics
Thursday, 26 April 2012 134-SDM-86
Akaka Falls
Waialua
Koko Crater
Molokai
51
Westlake, OH J. Wei, L. Dharani, K. Chandrashekhara, G. Hilmas, W. Fahrenholtz, Missouri University of Science and Technology, Rolla, MO
Chaired by: W. YU and L. DANIEL, Massachusetts Institute of Technology 1300 hrs 1330 hrs AIAA-2012-2000 AIAA-2012-2001 Modeling of Oxidation Effects on Heat Continuum Modeling of Synthetic Transfer Behavior of ZrB2 and ZrB2- Microvascular Materials G. Henson, Invariant Laboratories, LLC, SiC Ceramics at High Temperature
Thursday, 26 April 2012 139-SDM-91
F. Dervault, D. Lencz, Bombardier Aerospace, Montréal, Canada
Chaired by: J. WANG, Kingston University and E. ALTHOF, Raytheon Company 1300 hrs 1330 hrs AIAA-2012-1993 AIAA-2012-1995 Weight Investigation of a Novel Cabin Window Design Space Split-Wing Airplane Layout Exploration and Understanding W. Liu, B. Kaushik, W. Anemaat, of Interactions with Surrounding DARcorporation, Lawrence, KS Structure
Thursday, 26 April 2012 138-SDM-90
R. Heller, Southwest Research Institute, Hill AFB, UT; P. Clark, M. Thomsen, U.S. Air Force, Hill AFB, UT; T. Wilson, The Boeing Company, Saint Louis, MO
1430 hrs AIAA-2012-1997 Development of an Enhanced Wing for the A-10 Wing Replacement Program (WRP) R. Vos, F. Geuskens, Delft University of Technology, Delft, The Netherlands
1500 hrs AIAA-2012-1998 A New Structural Design Concept for Blended Wing Body Cabins
S. Godfrey, L. Valdevit, University of California, Irvine, Irvine, CA
1430 hrs AIAA-2012-2003 A Novel Modeling Platform for Characterization and Optimal Design of Micro-Architected Materials
Materials Model Development and Applications
Z. Ye, W. Yu, Utah State University, Logan, UT
1400 hrs AIAA-2012-2002 Maximize Unit Cell Choices for Variational Asymptotic Homogenization
G. Romanelli, T. Solcia, Technical University of Milan, Milan, Italy
1400 hrs AIAA-2012-1996 Multi-fidelity framework for the design and MSD/CFD verification of flutter suppression active control system
Design, Advanced Aircraft
V. Mukhopadhyay, NASA Langley Research Center, Hampton, VA
1530 hrs AIAA-2012-1999 Hybrid-Wing-Body Pressurized Fuselage Modeling, Analysis and Design for Weight Reduction
Kohala
Puna
52
Aarons, T., 84-SDM-57 Abbeel, P., 75-MDO-10 Abdelkefi, A., 98-SDM-65, 104-SDM-71 Abdi, F., 17-SDM-13 Abramson, D., 74-MDO-9 Abu-Zurayk, M., 92-MDO-12 Acar, E., 128-NDA-13 Acar, P., 99-SDM-66 Achuthan, A., 16-SDM-12 Adhikari, S., 137-SDM-89 Agnes, G., 89-ASC-5, 122-SDM-81 Agwai, A., 133-SDM-85 Ajaj, R., 37-ASC-1, 89-ASC-5 Akangah, P., 7-SDM-3 Alerding, J., 65-SDM-44 Alexandrov, N., 110-MDO-14 Allaire, D., 20-MDO-4, 110-MDO-14 Allcorn, E., 15-SDM-11 Allegri, G., 89-ASC-5 Allen, D., 7-SDM-3 Allen, M., 16-SDM-12, 116-SDM-75, 134-SDM-86 Allison, J., 40-MDO-7 Almer, J., 15-SDM-11 Alonso, J., 93-NDA-10 Alstrom, B., 30-SDM-22 Altenbuchner, C., 136-SDM-88 Althof, E., 84-SDM-57, 138-SDM-90 Alyanak, E., 19-MDO-3, 74-MDO-9 Ambur, D., 54-ASC-2 Ameri, N., 124-GSF-7 An, D., 21-NDA-3 Anderson, E., 68-SDM-47 Anderson, T., 20-MDO-4 Andrianne, T., 49-SDM-34, 99-SDM-66 Anemaat, W., 138-SDM-90 Anton, E., 74-MDO-9, 92-MDO-12 Antoun, B., 5-NDA-2 Antoun, G., 11-SDM-7 Aoki, T., 82-SDM-55 Apetre, N., 9-SDM-5, 86-SDM-59 Arcari, A., 9-SDM-5, 86-SDM-59 Ardelean, E., 131-SDM-83 Arena, A., 135-SDM-87 Aridon, G., 51-SDM-36 Armanios, E., 130-SDM-82 Arnold, S., 24-SDM-16, 45-SDM-30, 133-SDM-85 Arrieta, A., 89-ASC-5 Arritt, B., 55-GSF-2, 89-ASC-5 Arsenault, T., 16-SDM-12 Asareh, M., 104-SDM-71
Asheghian, L., 136-SDM-88 Ashrafi, B., 85-SDM-58 Ashwill, T., 33-SDM-25, 104-SDM-71 Askari, A., 122-SDM-81 Atcheson, P., 73-GSF-3 Attar, P., 82-SDM-55 Avila, A., 15-SDM-11, 67-SDM-46 Azevedo, J., 83-SDM-56 Babuska, V., 58-NDA-8, 63-SDM-42, 66-SDM-45, 129-NDA-14 Badcock, K., 49-SDM-34, 81-SDM-54 Badran, O., 98-SDM-65 Baeder, J., 65-SDM-44 Baek, M., 15-SDM-11 Bai, T., 137-SDM-89 Baier, H., 89-ASC-5 Bailey, M., 84-SDM-57 Bak, C., 33-SDM-25 Bakalyar, J., 123-ASC-7 Bakis, C., 94-SDM-61 Balabanov, V., 36-MDO-5, 39-MDO-6, 62-SDM-41, 113-SDM-72 Baldomir, A., 60-SDM-39, 75-MDO-10, 91-MDO-11 Ball, D., 14-SDM-10 Band, J., 10-SDM-6, 137-SDM-89 Bandyopadhyay, A., 85-SDM-58 Banerjee, J., 28-SDM-20 Banik, J., 55-GSF-2, 108-GSF-6, 131-SDM-83 Banker, M., 6-SDM-2 Bansal, P., 99-SDM-66 Barbarino, S., 82-SDM-55 Barber, D., 38-GSF-1 Barnhart, R., 37-ASC-1, 123-ASC-7 Barone, M., 104-SDM-71 Barrett, R., 123-ASC-7 Barrett-Gonzalez, R., 37-ASC-1 Bartels, R., 64-SDM-43 Bartram, G., 4-NDA-1 Barut, A., 44-SDM-29, 80-SDM-53 Basiricò, L., 67-SDM-46 Batra, R., 78-SDM-51 Baum, J., 117-SDM-76 Becz, S., 79-SDM-52 Bednarcyk, B., 24-SDM-16, 43-SDM-28, 45-SDM-30, 60-SDM-39, 133-SDM-85 Beldica, C., 115-SDM-74 Bell, C., 89-ASC-5 Belvin, W., 131-SDM-83 Ben Ayed, S., 129-NDA-14 Bendiksen, O., 83-SDM-56
Author/Session Chair Index Benedict, M., 64-SDM-43, 65-SDM-44 Beran, P., 3-MDO-2, 65-SDM-44 Berci, M., 95-SDM-62 Bergman, D., 124-GSF-7 Bernier, A., 119-SDM-78 Bernstein, D., 29-SDM-21 Bernstein, K., 95-SDM-62 Bersee, H., 24-SDM-16 Bes, C., 58-NDA-8 Bestard, J., 34-SDM-26 Betts, D., 31-SDM-23 Bhasin, S., 98-SDM-65 Bhatia, M., 99-SDM-66 Bianchi, F., 24-SDM-16 Bichiou, Y., 69-SDM-48 Bichon, B., 129-NDA-14 Biester, M., 70-SDM-49 Biggs, R., 94-SDM-61 Biggs, S., 51-SDM-36 Bijl, H., 112-NDA-12 Bilgen, O., 123-ASC-7 Birkefeld, K., 120-SDM-79 Bisagni, C., 8-SDM-4, 115-SDM-74 Black, J., 65-SDM-44, 84-SDM-57 Blain, A., 37-ASC-1 Blom, A., 39-MDO-6 Bloomhardt, L., 100-SDM-67 Boekeloo, E., 92-MDO-12 Bogert, P., 62-SDM-41 Bogge, M., 77-SDM-50 Boles, T., 96-SDM-63 Bolinches i Gisbert, M., 84-SDM-57 Bombardier, Y., 79-SDM-52 Bonacuse, P., 68-SDM-47 Bonakdar, M., 50-SDM-35 Bond, I., 67-SDM-46 Boonen, R., 86-SDM-59 Borkowski, L., 97-SDM-64 Boscolo, M., 28-SDM-20, 79-SDM-52 Botez, R., 89-ASC-5 Bourgeois, S., 131-SDM-83 Bowen, C., 31-SDM-23 Bower, G., 40-MDO-7 Bradford, S., 89-ASC-5 Bramlette, R., 37-ASC-1 Brandyberry, M., 102-SDM-69 Breitzman, T., 68-SDM-47 Brezillon, J., 92-MDO-12, 109-MDO-13 Bridges, R., 14-SDM-10 Briggs, H., 101-SDM-68
Brinkmeyer, A., 54-ASC-2 Britt, R., 27-SDM-19 Brockman, R., 62-SDM-41 Brodersen, O., 109-MDO-13 Bron, F., 132-SDM-84 Brown, A., 12-SDM-8 Brown, G., 38-GSF-1, 70-SDM-49 Brown, R., 32-SDM-24 Bruno, E., 95-SDM-62 Bruun, E., 79-SDM-52 Buck, M., 34-SDM-26 Buckney, N., 33-SDM-25 Budinger, M., 40-MDO-7 Buede, D., 41-NDA-5 Bull, K., 2-MDO-1 Busch, G., 42-SDM-27 Bushnell, D., 23-SDM-15 Butler, R., 26-SDM-18 Butt, L., 99-SDM-66 Cadièrgues, L., 51-SDM-36 Cairns, D., 17-SDM-13 Cammarano, A., 134-SDM-86 Campo, L., 22-NDA-4 Canfield, R., 19-MDO-3, 25-SDM-17, 83-SDM-56, 84-SDM-57, 126-MDO-15 Capellaro, M., 33-SDM-25 Capps, R., 37-ASC-1 Cardenas Fuentes, D., 17-SDM-13 Carlberg, K., 134-SDM-86 Carponcin, D., 51-SDM-36 Carr, R., 2-MDO-1 Carrella, A., 134-SDM-86 Carrera, E., 59-SDM-38, 78-SDM-51 Carrier, G., 126-MDO-15 Castellani, M., 49-SDM-34 Castillo, L., 2-MDO-1 Catalano, M., 2-MDO-1 Cattan, E., 65-SDM-44 Causse, N., 51-SDM-36 Cavallaro, R., 26-SDM-18 Cebeci, H., 8-SDM-4, 50-SDM-35 Ceisel, J., 91-MDO-11 Centea, T., 51-SDM-36 Cesnik, C., 10-SDM-6, 81-SDM-54, 82-SDM-55, 109-MDO-13, 135-SDM-87, 136-SDM-88 Chakravarty, U., 136-SDM-88 Chamis, C., 45-SDM-30, 58-NDA-8, 61-SDM-40 Chan, S., 50-SDM-35 Chandraseker, K., 17-SDM-13 Chandrashekhara, K., 139-SDM-91
Chang, F., 102-SDM-69 Chattopadhyay, A., 44-SDM-29, 61-SDM-40, 97-SDM-64, 130-SDM-82, 133-SDM-85 Chaudhuri, A., 75-MDO-10 Chen, D., 91-MDO-11, 132-SDM-84 Chen, L., 27-SDM-19 Chen, M., 67-SDM-46, 122-SDM-81 Chen, P., 47-SDM-32, 49-SDM-34, 74-MDO-9, 98SDM-65, 101-SDM-68, 104-SDM-71 Chen, W., 121-SDM-80 Chen, Y., 29-SDM-21 Chen, Z., 61-SDM-40 Cheng, G., 56-MDO-8 Chennimalai Kumar, N., 40-MDO-7 Chessa, J., 79-SDM-52 Cheung, C., 120-SDM-79 Chevalier, M., 51-SDM-36 Chierichetti, M., 137-SDM-89 Chishiki, Y., 90-GSF-4 Cho, C., 107-ASC-6 Cho, M., 43-SDM-28, 103-SDM-70 Choi, J., 21-NDA-3, 93-NDA-10, 103-SDM-70, 129-NDA-14 Choi, S., 57-NDA-7, 109-MDO-13 Chopra, I., 28-SDM-20, 48-SDM-33, 64-SDM-43, 65-SDM-44, 72-ASC-4, 84-SDM-57 Chowdhury, S., 2-MDO-1, 20-MDO-4, 40-MDO-7, 75-MDO-10, 127-MDO-16 Christensen, S., 31-SDM-23 Christhilf, D., 47-SDM-32 Christodoulou, J., 14-SDM-10 Chunchu, P., 77-SDM-50 Chung, C., 136-SDM-88 Chung, J., 21-NDA-3 Chung, Y., 11-SDM-7, 63-SDM-42 Ciampa, P., 126-MDO-15 Cinefra, M., 59-SDM-38 Cizmas, P., 32-SDM-24 Clark, B., 94-SDM-61 Clark, P., 138-SDM-90 Clay, S., 43-SDM-28, 58-NDA-8, 120-SDM-79 Cochelin, B., 131-SDM-83 Cochran, R., 94-SDM-61 Colavito, K., 44-SDM-29 Cole, D., 51-SDM-36 Cole, S., 46-SDM-31 Combes, H., 51-SDM-36 Congedo, P., 76-NDA-9 Connell, J., 131-SDM-83 Conte, J., 4-NDA-1
53
Cook, T., 14-SDM-10 Cooley, P., 116-SDM-75 Cooper, B., 131-SDM-83 Cooper, J., 25-SDM-17, 27-SDM-19, 30-SDM-22, 48-SDM-33 Cope, D., 21-NDA-3, 97-SDM-64 Copeland, S., 93-NDA-10 Coppotelli, G., 12-SDM-8, 16-SDM-12 Cormier, L., 52-SDM-37 Corson, D., 104-SDM-71 Cortial, J., 134-SDM-86 Cortina, M., 112-NDA-12 Cosentino, E., 61-SDM-40, 115-SDM-74 Costantine, J., 108-GSF-6 Cotton, J., 14-SDM-10 Coulson, D., 47-SDM-32 Cox, J., 63-SDM-42 Coyne, B., 137-SDM-89 Cozmuta, I., 93-NDA-10 Craigmyle, B., 66-SDM-45 Crawford, C., 33-SDM-25, 56-MDO-8 Cregger, S., 39-MDO-6 Crespo, L., 20-MDO-4, 111-NDA-11 Crisafulli, D., 59-SDM-38 Cross, D., 126-MDO-15 Crouch, R., 43-SDM-28 Culler, A., 102-SDM-69, 117-SDM-76 Culler, E., 84-SDM-57 Curtis, P., 117-SDM-76 Curtis, S., 110-MDO-14 Cushman, A., 11-SDM-7 Cutshall, J., 101-SDM-68 Cwik, T., 117-SDM-76 Czarnecki, G., 34-SDM-26 da Silva, R., 135-SDM-87 Dai, Y., 27-SDM-19 Dande, H., 28-SDM-20 Dandurand, J., 51-SDM-36 Daniel, L., 139-SDM-91 Dantras, E., 51-SDM-36 Daraio, C., 10-SDM-6 Das, K., 32-SDM-24 Das, S., 4-NDA-1 Datashvili, L., 55-GSF-2 Daton-Lovett, A., 90-GSF-4 Dauwalter, C., 101-SDM-68 Davidson, P., 17-SDM-13 Davis, C., 21-NDA-3 Davis, G., 122-SDM-81, 124-GSF-7, 125-GSF-8 Davis, J., 13-SDM-9
Daynes, S., 72-ASC-4 de Avila, Jr., J., 15-SDM-11 De Marqui Jr., C., 72-ASC-4 de Souza, C., 135-SDM-87 de Souza, D., 15-SDM-11 Deaner, B., 134-SDM-86 Deaton, J., 91-MDO-11 Defrancisci, G., 61-SDM-40 Deloo, P., 95-SDM-62 Demasi, L., 8-SDM-4, 26-SDM-18, 98-SDM-65, 130-SDM-82 Dempsey, F., 5-NDA-2 Deng, S., 68-SDM-47 Dervault, F., 138-SDM-90 Desideri, J., 126-MDO-15 Desmet, W., 87-SDM-60 Dettmer, W., 89-ASC-5 Dhainaut, J., 98-SDM-65, 99-SDM-66 Dharani, L., 139-SDM-91 Di Maio, D., 124-GSF-7 Di Matteo, N., 60-SDM-39 Diaz, J., 3-MDO-2, 60-SDM-39, 75-MDO-10, 91-MDO-11 Didion, J., 42-SDM-27 Dillman, R., 38-GSF-1 Dimitriadis, G., 27-SDM-19, 49-SDM-34, 81-SDM-54, 99-SDM-66 Dinavahi, S., 30-SDM-22 Diner, A., 104-SDM-71 Dixit, A., 116-SDM-75 Dizy, J., 130-SDM-82 Doane, N., 42-SDM-27 Doggett, W., 95-SDM-62 Doman, D., 136-SDM-88 Domb, M., 23-SDM-15, 95-SDM-62 Domber, J., 73-GSF-3, 131-SDM-83 Domyancic, L., 112-NDA-12 Dorman, P., 109-MDO-13 DorMohammadi, S., 110-MDO-14 Dorobantu, A., 20-MDO-4 Dowell, E., 64-SDM-43, 100-SDM-67 Dowling, N., 86-SDM-59 Doyle, D., 42-SDM-27, 55-GSF-2, 89-ASC-5 Drake, D., 86-SDM-59 Drechsler, K., 120-SDM-79, 121-SDM-80 Dribusch, C., 100-SDM-67 Duan, K., 74-MDO-9 Dubinsky, C., 129-NDA-14 Duffy, K., 66-SDM-45 Duggirala, V., 91-MDO-11
Author/Session Chair Index Dumont, A., 126-MDO-15 Dunn, M., 9-SDM-5 Dunning, P., 56-MDO-8 Durin, C., 51-SDM-36 Durmaz, S., 135-SDM-87 Dwight, R., 112-NDA-12 D`souza, K., 98-SDM-65 Díaz De la O, F., 68-SDM-47 Eaton, J., 22-NDA-4 Ehlert, G., 15-SDM-11 El Arras, A., 136-SDM-88 El Halabi, T., 40-MDO-7 Eldred, M., 76-NDA-9, 111-NDA-11 Elizalde, H., 17-SDM-13 Elliott, K., 96-SDM-63, 131-SDM-83 Embley, M., 132-SDM-84 Engelsen, F., 126-MDO-15 Engelstad, S., 24-SDM-16, 45-SDM-30 Enright, M., 9-SDM-5, 41-NDA-5, 129-NDA-14 Epton, M., 39-MDO-6 Epureanu, B., 98-SDM-65 Erford, M., 38-GSF-1 Eslami, H., 99-SDM-66 Esmailzadeh, E., 107-ASC-6 Eun, W., 72-ASC-4 Evuri, A., 66-SDM-45 Ewing, M., 28-SDM-20 Ewins, D., 124-GSF-7 Fahrenholtz, W., 139-SDM-91 Fahrenthold, E., 34-SDM-26 Faidi, W., 17-SDM-13 Fairbairn, B., 94-SDM-61 Fang, H., 73-GSF-3, 108-GSF-6, 124-GSF-7 Farhat, C., 134-SDM-86 Farmer, B., 85-SDM-58, 103-SDM-70 Favaloro, A., 92-MDO-12 Fazzolari, F., 28-SDM-20 Fefey, E., 103-SDM-70 Fehrman, B., 11-SDM-7 Fernandez, J., 90-GSF-4, 131-SDM-83 Fernandez Villegas, I., 24-SDM-16 Ferraro, M., 84-SDM-57, 101-SDM-68 Fertig, R., 68-SDM-47 Field, T., 15-SDM-11 Fischer, G., 2-MDO-1 Fischer, M., 2-MDO-1 Fitch, S., 41-NDA-5 Fitspatrick, I., 25-SDM-17 Fitzwater, L., 21-NDA-3 Flatau, A., 107-ASC-6
Florance, J., 47-SDM-32 Foerster, C., 118-SDM-77 Foo, J., 40-MDO-7 Footdale, J., 11-SDM-7, 131-SDM-83 Forrester, A., 127-MDO-16 Forslund, A., 101-SDM-68 Fraj, A., 40-MDO-7 Francis, A., 7-SDM-3 Franz, K., 74-MDO-9, 92-MDO-12 Friedl, F., 2-MDO-1 Friedmann, P., 29-SDM-21, 66-SDM-45 Friswell, M., 37-ASC-1, 68-SDM-47, 89-ASC-5, 123-ASC-7 Frohlich, C., 14-SDM-10 Fulcher, C., 63-SDM-42 Funase, R., 90-GSF-4 Funk, C., 47-SDM-32 Furrer, D., 31-SDM-23 Furuya, H., 125-GSF-8 Gaitonde, D., 30-SDM-22 Gallegos, A., 4-NDA-1 Gandhi, F., 82-SDM-55 Gangadharan, S., 119-SDM-78 Garnand-Royo, J., 84-SDM-57 Garnich, M., 68-SDM-47 Garvin, C., 7-SDM-3, 132-SDM-84 Gelhausen, P., 37-ASC-1 George, T., 66-SDM-45 Georgiou, G., 25-SDM-17 Gern, F., 60-SDM-39 Geubelle, P., 32-SDM-24 Geuskens, F., 138-SDM-90 Ghanem, R., 4-NDA-1, 41-NDA-5, 69-SDM-48 Ghazlane, I., 126-MDO-15 Ghisu, T., 19-MDO-3 Ghoman, S., 101-SDM-68 Ghommem, M., 69-SDM-48, 136-SDM-88 Gibbs IV, S., 100-SDM-67 Giesy, D., 111-NDA-11 Giurgiutiu, V., 31-SDM-23 Glaessgen, E., 15-SDM-11, 50-SDM-35, 85-SDM-58, 102-SDM-69, 103-SDM-70 Glavicic, M., 31-SDM-23 Glaz, B., 30-SDM-22 Glazebrook, C., 132-SDM-84 Gobbato, M., 4-NDA-1 Gockel, B., 102-SDM-69 Godfrey, S., 139-SDM-91 Gogu, C., 58-NDA-8 Goldberg, R., 68-SDM-47
Golden, P., 12-SDM-8, 58-NDA-8, 129-NDA-14 Gordnier, R., 65-SDM-44, 83-SDM-56 Gordon, R., 46-SDM-31 Gorissen, D., 84-SDM-57, 101-SDM-68 Goyal, V., 6-SDM-2, 61-SDM-40, 78-SDM-51, 95SDM-62, 113-SDM-72 Graham, J., 7-SDM-3, 30-SDM-22 Grandhi, R., 20-MDO-4, 91-MDO-11, 93-NDA-10, 111-NDA-11, 112-NDA-12 Grappasogni, C., 16-SDM-12 Grappasonni, C., 12-SDM-8 Grasso, F., 2-MDO-1 Graves, R., 112-NDA-12 Gray, J., 56-MDO-8, 74-MDO-9 Gray, P., 120-SDM-79 Graybeal, N., 64-SDM-43 Green, S., 33-SDM-25 Greenhalgh, E., 7-SDM-3 Grenoble, R., 94-SDM-61, 113-SDM-72 Greschik, G., 73-GSF-3, 90-GSF-4 Griffin, K., 94-SDM-61 Griffith, D., 16-SDM-12, 33-SDM-25, 52-SDM-37, 104-SDM-71 Grobler, F., 73-GSF-3 Grondel, S., 65-SDM-44 Grosbein, H., 45-SDM-30 Guan, X., 57-NDA-7 Gubel, A., 73-GSF-3 Guendogdu, Y., 70-SDM-49 Guerrant, D., 90-GSF-4 Guigue, P., 51-SDM-36 Guimard, J., 78-SDM-51 Guinot, F., 131-SDM-83 Gunel, M., 113-SDM-72 Guo, C., 19-MDO-3 Guo, S., 37-ASC-1, 60-SDM-39 Guo, Y., 16-SDM-12 Gupta, V., 85-SDM-58 Gurtowski, N., 99-SDM-66 Guruswamy, G., 49-SDM-34 Gustafson, P., 6-SDM-2, 43-SDM-28, 59-SDM-38 Guven, I., 44-SDM-29, 133-SDM-85 Guzman, J., 77-SDM-50 Guzman de Villoria, R., 8-SDM-4, 50-SDM-35 Gwaltney, S., 85-SDM-58 Haar, D., 92-MDO-12 Hadadian, A., 107-ASC-6 Haftka, R., 57-NDA-7, 58-NDA-8, 75-MDO-10, 111-NDA-11, 112-NDA-12, 128-NDA-13 Hagedorn, P., 89-ASC-5
54
Haile, M., 51-SDM-36 Haji Hajikolaei, K., 127-MDO-16 Hajj, M., 69-SDM-48, 98-SDM-65, 104-SDM-71, 129-NDA-14, 136-SDM-88 Halbert, K., 21-NDA-3 Hall, A., 51-SDM-36 Hall, K., 137-SDM-89 Hallander, P., 50-SDM-35 Hancock, B., 110-MDO-14 Hanson, J., 94-SDM-61 Hardaway, L., 26-SDM-18 Harding, A., 11-SDM-7 Harish, A., 115-SDM-74 Harper, D., 114-SDM-73 Harris, T., 92-MDO-12 Hart, R., 8-SDM-4 Harte, M., 16-SDM-12 Harursampath, D., 6-SDM-2, 10-SDM-6, 115-SDM-74, 133-SDM-85 Haynie, W., 77-SDM-50 He, J., 57-NDA-7 He, Q., 20-MDO-4 Heath, C., 56-MDO-8, 74-MDO-9 Hebert, C., 64-SDM-43 Heeg, J., 13-SDM-9 Heinrich, C., 43-SDM-28 Helgesen, B., 23-SDM-15 Heller, R., 138-SDM-90 Helmer, D., 22-NDA-4 Helsen, J., 87-SDM-60 Hemez, F., 69-SDM-48 Hengeveld, D., 42-SDM-27 Henke, M., 70-SDM-49 Henry, E., 38-GSF-1 Henson, G., 6-SDM-2, 139-SDM-91 Hepperle, M., 109-MDO-13 Hernandez, S., 60-SDM-39, 75-MDO-10, 91-MDO- 11, 92-MDO-12 Herrera, C., 11-SDM-7 Herring, H., 77-SDM-50 Heslehurst, R., 121-SDM-80 Hesse, H., 13-SDM-9 Hickling, C., 37-ASC-1 Hiemenz, G., 117-SDM-76 Hilburger, M., 77-SDM-50, 114-SDM-73 Hillebrandt, M., 55-GSF-2 Hilmas, G., 139-SDM-91 Hilton, H., 25-SDM-17, 45-SDM-30, 86-SDM-59, 94-SDM-61 Hinkle, J., 38-GSF-1 Hinrichsen, R., 34-SDM-26 Hobeck, J., 118-SDM-77 Hoburg, W., 75-MDO-10 Hochhalter, J., 85-SDM-58 Hodges, D., 64-SDM-43, 116-SDM-75, 132-SDM-84 Hoernschemeyer, R., 74-MDO-9, 92-MDO-12 Hoffman, S., 89-ASC-5 Hofmann, D., 122-SDM-81 Hollenbeck, A., 8-SDM-4 Hollkamp, J., 46-SDM-31 Holloway, N., 131-SDM-83 Holub, J., 40-MDO-7 Hombal, V., 44-SDM-29, 75-MDO-10 Hombergsmeier, E., 121-SDM-80 Honea, G., 70-SDM-49 Hong, J., 93-NDA-10 Hoos, K., 68-SDM-47 Hootsmans, L., 101-SDM-68 Hornung, M., 89-ASC-5 Horta, L., 125-GSF-8 Houston, G., 132-SDM-84 Hrinda, G., 59-SDM-38, 97-SDM-64 Hrishikeshavan, V., 84-SDM-57 Hu, C., 21-NDA-3, 70-SDM-49 Hu, H., 10-SDM-6 Hu, K., 58-NDA-8 Hu, W., 117-SDM-76 Hubbard, J., 136-SDM-88 Hubert, P., 51-SDM-36 Huehne, C., 55-GSF-2 Hughes, S., 51-SDM-36 Humphrey, L., 92-MDO-12 Hunt, J., 7-SDM-3, 24-SDM-16 Hunt, R., 63-SDM-42, 66-SDM-45 Hunter, N., 22-NDA-4 Hur, H., 130-SDM-82 Hur, J., 47-SDM-32 Hurtado, J., 30-SDM-22 Hussien, A., 94-SDM-61 Hutchinson, S., 37-ASC-1 Hwang, J., 56-MDO-8 Hyer, M., 132-SDM-84 Iaccarino, G., 5-NDA-2, 22-NDA-4, 76-NDA-9 Iannucci, L., 117-SDM-76 Iarve, E., 62-SDM-41, 68-SDM-47 Ibrahimoglu, S., 28-SDM-20 Ide, K., 82-SDM-55 Ifju, P., 123-ASC-7 Ihn, J., 21-NDA-3 Imperiale, V., 67-SDM-46
Author/Session Chair Index Inman, D., 31-SDM-23, 48-SDM-33, 50-SDM-35, 118-SDM-77 Iovnovich, M., 64-SDM-43 Ishiguro, K., 50-SDM-35 Isikveren, A., 89-ASC-5 Iyyer, N., 9-SDM-5, 86-SDM-59 Jacob, J., 136-SDM-88 Jakubinek, M., 85-SDM-58 Janapati, V., 102-SDM-69 Jang, C., 85-SDM-58 Jansz, M., 15-SDM-11 Jarugumilli, T., 64-SDM-43 Jaworski, J., 65-SDM-44 Jenkins, C., 73-GSF-3, 124-GSF-7, 125-GSF-8 Jennings, A., 65-SDM-44 Jensen, D., 7-SDM-3, 132-SDM-84 Jensen, M., 7-SDM-3, 132-SDM-84 Jeon, S., 11-SDM-7, 23-SDM-15, 131-SDM-83 Jha, R., 54-ASC-2, 57-NDA-7 Ji, W., 45-SDM-30 Jia, Z., 109-MDO-13 Jing, Z., 27-SDM-19 Johann, E., 93-NDA-10 Johannesson, H., 101-SDM-68 John, R., 58-NDA-8, 102-SDM-69 Johnson, B., 15-SDM-11, 92-MDO-12 Johnson, D., 11-SDM-7, 29-SDM-21 Johnson, E., 78-SDM-51 Johnson, H., 46-SDM-31 Johnson, T., 118-SDM-77 Johnston, A., 85-SDM-58 Jones, A., 15-SDM-11 Jones, D., 21-NDA-3 Jones, R., 8-SDM-4 Jones, T., 95-SDM-62, 118-SDM-77 Jonkman, J., 87-SDM-60 Jorris, T., 2-MDO-1 Joshi, P., 63-SDM-42 Jou, H., 31-SDM-23 Jun, S., 109-MDO-13 Jung, B., 107-ASC-6 Jung, C., 98-SDM-65 Jurewicz, D., 38-GSF-1 Jutte, C., 123-ASC-7 Kalamoun, S., 50-SDM-35 Kalivarapu, V., 40-MDO-7 Kanakasabai, P., 3-MDO-2 Kang, K., 129-NDA-14 Kang, P., 9-SDM-5, 86-SDM-59 Kang, Y., 109-MDO-13
Kapania, R., 3-MDO-2, 63-SDM-42, 74-MDO-9, 78-SDM-51, 80-SDM-53, 91-MDO-11, 99-SDM-66, 101-SDM-68, 132-SDM-84 Karakaya, S., 108-GSF-6 Karayev, K., 62-SDM-41, 113-SDM-72 Karni, E., 37-ASC-1 Karpel, M., 13-SDM-9, 100-SDM-67 Katsumata, N., 55-GSF-2 Kauffman, J., 66-SDM-45 Kaushik, B., 138-SDM-90 Kawaguchi, J., 90-GSF-4 Kaya, M., 66-SDM-45, 135-SDM-87 Kayran, A., 28-SDM-20, 113-SDM-72 Keane, A., 84-SDM-57, 101-SDM-68, 127-MDO-16 Kecskemety, K., 104-SDM-71 Kelkar, A., 51-SDM-36, 103-SDM-70 Keller, D., 47-SDM-32 Kelley, C., 38-GSF-1 Kemp, J., 34-SDM-26 Kenik, D., 62-SDM-41, 113-SDM-72 Kennedy, D., 6-SDM-2 Kennedy, G., 39-MDO-6, 126-MDO-15 Kennedy, T., 62-SDM-41 Kenny, S., 111-NDA-11 Kenway, G., 126-MDO-15 Keskin, A., 14-SDM-10 Khan, A., 78-SDM-51 Khemani, F., 43-SDM-28 Khodaparast, H., 48-SDM-33 Kier, Z., 113-SDM-72 Kim, D., 37-ASC-1, 83-SDM-56 Kim, H., 7-SDM-3, 26-SDM-18, 31-SDM-23, 56-MDO-8, 61-SDM-40, 74-MDO-9 Kim, J., 93-NDA-10, 115-SDM-74, 118-SDM-77 Kim, K., 93-NDA-10 Kim, N., 13-SDM-9, 21-NDA-3, 57-NDA-7, 58-NDA-8, 112-NDA-12, 133-SDM-85 Kim, T., 21-NDA-3, 33-SDM-25 Kim, W., 93-NDA-10 Kim, Y., 83-SDM-56, 107-ASC-6, 113-SDM-72, 125-GSF-8, 129-NDA-14 Kinney, T., 119-SDM-78 Kipouros, T., 2-MDO-1, 19-MDO-3, 74-MDO-9 Kitamura, K., 90-GSF-4 Kloos, J., 34-SDM-26 Knight, N., 96-SDM-63, 131-SDM-83 Kobayashi, M., 3-MDO-2 Koch, R., 78-SDM-51, 130-SDM-82 Kocher, B., 34-SDM-26 Kochersberger, K., 37-ASC-1
Kogiso, N., 108-GSF-6 Kolonay, R., 30-SDM-22 Kolsti, K., 134-SDM-86 Koo, J., 15-SDM-11, 103-SDM-70 Korde, U., 11-SDM-7, 66-SDM-45 Kosmatka, J., 4-NDA-1, 24-SDM-16, 82-SDM-55, 97-SDM-64, 118-SDM-77 Kothera, C., 38-GSF-1, 72-ASC-4 Krattiger, D., 58-NDA-8 Kratz, J., 51-SDM-36 Krebs, D., 63-SDM-42 Kreshock, A., 29-SDM-21 Kriegesmann, B., 77-SDM-50, 114-SDM-73 Krishnamurthy, T., 4-NDA-1 Kroo, I., 19-MDO-3, 40-MDO-7 Kruth, J., 86-SDM-59 Kuehmann, C., 31-SDM-23 Kuether, R., 134-SDM-86 Kukreja, S., 99-SDM-66 Kumar, D., 109-MDO-13 Kumari, S., 44-SDM-29 Kundu, A., 137-SDM-89 Kunz, D., 134-SDM-86 Kwok, K., 124-GSF-7 Labryer, A., 82-SDM-55 Lacabanne, C., 51-SDM-36 Lacarbonara, W., 135-SDM-87 LaCava, W., 16-SDM-12 Lacaze, S., 20-MDO-4 LaCroix, B., 123-ASC-7 Lacy, S., 58-NDA-8, 129-NDA-14 Lacy, T., 26-SDM-18, 85-SDM-58, 103-SDM-70, 133-SDM-85 Ladesic, J., 99-SDM-66 Laffont, L., 51-SDM-36 Lagoudas, D., 32-SDM-24 Lai, K., 81-SDM-54 Lake, C., 15-SDM-11 Lake, P., 15-SDM-11 Lake, T., 92-MDO-12 Lakis, A., 81-SDM-54 Lakshminarayan, V., 65-SDM-44 Lamberson, S., 100-SDM-67 Lammering, T., 74-MDO-9, 92-MDO-12 Lane, S., 58-NDA-8 Lange, A., 93-NDA-10 Langelaar, M., 3-MDO-2 Langford, W., 120-SDM-79 Langston, C., 29-SDM-21 Lanzara, G., 67-SDM-46
55
Lao, S., 15-SDM-11 Lappas, V., 90-GSF-4 Laue, G., 38-GSF-1 Laun, F., 42-SDM-27 LaVerde, B., 63-SDM-42, 66-SDM-45 Lawrence, D., 90-GSF-4 Lazansky, C., 23-SDM-15 Le Riche, R., 128-NDA-13 Lee, C., 84-SDM-57 Lee, D., 94-SDM-61, 109-MDO-13, 129-NDA-14 Lee, E., 12-SDM-8 Lee, H., 3-MDO-2 Lee, J., 70-SDM-49, 72-ASC-4, 93-NDA-10, 103-SDM-70, 109-MDO-13 Lee, M., 91-MDO-11 Lee, P., 118-SDM-77 Lee, S., 3-MDO-2, 62-SDM-41, 109-MDO-13, 113-SDM-72 Leem, S., 21-NDA-3 Lenahen, B., 119-SDM-78 Lencz, D., 138-SDM-90 Lepsch, R., 2-MDO-1 Lesieutre, G., 66-SDM-45, 116-SDM-75 Lester, B., 32-SDM-24 Leuva, D., 119-SDM-78 Levallois, F., 51-SDM-36 Levandowski, C., 101-SDM-68 Lewis, P., 110-MDO-14 Li, G., 46-SDM-31 Li, H., 102-SDM-69 Li, J., 133-SDM-85 Li, Q., 137-SDM-89 Li, V., 39-MDO-6 Li, Y., 103-SDM-70 Liang, C., 75-MDO-10 Liang, W., 41-NDA-5 Liao, M., 79-SDM-52 Lichodziejewski, D., 38-GSF-1, 108-GSF-6 Lieser, J., 109-MDO-13 Liguore, S., 63-SDM-42 Lih, S., 11-SDM-7 Liiu, Y., 25-SDM-17 Lim, C., 129-NDA-14 Limer, T., 14-SDM-10 Lin, H., 41-NDA-5 Lin, J., 38-GSF-1, 108-GSF-6 Lin, K., 79-SDM-52, 94-SDM-61, 120-SDM-79 Lind, R., 63-SDM-42 Lindsley, N., 25-SDM-17 Ling, Y., 5-NDA-2, 44-SDM-29
Link, H., 16-SDM-12 Lippl, F., 70-SDM-49 Little, O., 37-ASC-1 Liu, D., 39-MDO-6, 120-SDM-72 Liu, K., 130-SDM-82 Liu, L., 79-SDM-52 Liu, S., 19-MDO-3 Liu, W., 26-SDM-18, 138-SDM-90 Liu, Y., 24-SDM-16, 57-NDA-7, 68-SDM-47, 86-SDM-59, 97-SDM-64, 102-SDM-69, 133-SDM-85 Livne, E., 49-SDM-34 Lo, H., 132-SDM-84 Locatelli, D., 3-MDO-2, 74-MDO-9 Loh, W., 136-SDM-88 Lohner, R., 117-SDM-76 Lomov, S., 129-NDA-14 Lonkar, K., 102-SDM-69 Lovejoy, A., 77-SDM-50, 114-SDM-73 Lu, Z., 68-SDM-47, 86-SDM-59 Lua, J., 79-SDM-52 Luber, W., 99-SDM-66 Lubineau, G., 122-SDM-81 Lum, K., 81-SDM-54 Lummer, M., 92-MDO-12 Lundgren, E., 23-SDM-15, 94-SDM-61 Luo, C., 44-SDM-29 Luo, W., 41-NDA-5 Luraghi, F., 6-SDM-2 Lurati, L., 111-NDA-11 Lyle, K., 125-GSF-8 Maasha, R., 11-SDM-7 Mabson, G., 39-MDO-6, 62-SDM-41 Madenci, E., 44-SDM-29, 78-SDM-51, 80-SDM-53, 130-SDM-82, 133-SDM-85 Mader, C., 92-MDO-12 Maggiore, P., 127-MDO-16 Mahadevan, S., 4-NDA-1, 5-NDA-2, 44-SDM-29, 75-MDO-10, 93-NDA-10, 102-SDM-69 Mahler, M., 133-SDM-85 Mahoney, S., 41-NDA-5 Maiarù, M., 78-SDM-51 Maier, H., 31-SDM-23 Mainini, L., 127-MDO-16 Malhan, R., 65-SDM-44 Mandell, J., 17-SDM-13, 52-SDM-37 Mann, T., 94-SDM-61 Manuel, L., 87-SDM-60, 104-SDM-71 Maqueda, I., 124-GSF-7 Marcelet, M., 126-MDO-15 Mardanpour, P., 64-SDM-43
Author/Session Chair Index Mare, J., 40-MDO-7 Mares, C., 89-ASC-5 Marques, F., 98-SDM-65 Marques, S., 81-SDM-54 Martinez-Rubi, Y., 85-SDM-58 Martins, J., 39-MDO-6, 56-MDO-8, 92-MDO-12, 126-MDO-15 Marzocca, P., 16-SDM-12, 17-SDM-13, 135-SDM-87 Masarati, P., 65-SDM-44 Mason, B., 94-SDM-61 Maspoli, M., 77-SDM-50 Mass, E., 70-SDM-49 Masuda, K., 132-SDM-84 Matlik, J., 14-SDM-10, 31-SDM-23, 41-NDA-5 Matney, A., 134-SDM-86 Matsumura, T., 112-NDA-12 Matsuzaki, Y., 117-SDM-76 Mattson, C., 20-MDO-4, 110-MDO-14 Matunaga, S., 90-GSF-4 Mauch, N., 10-SDM-6 Mavris, D., 91-MDO-11, 128-NDA-13 Mc Tigue, J., 27-SDM-19 Mcatee, C., 92-MDO-12 McCarville, D., 77-SDM-50 McClung, R., 41-NDA-5 McCrink, M., 30-SDM-22 McDaniel, D., 100-SDM-67 McDonald, E., 63-SDM-42 McDonough, L., 30-SDM-22 Mcfarland, J., 21-NDA-3 McGowan, D., 37-ASC-1 McLendon, W., 32-SDM-24 McNamara, J., 46-SDM-31, 104-SDM-71 McNiff, B., 16-SDM-12 McQuigg, T., 80-SDM-53 McWilliam, M., 33-SDM-25 Meehan, E., 73-GSF-3 Meguid, S., 81-SDM-54 Meidani, H., 69-SDM-48 Mejia-Ariza, J., 124-GSF-7 Merrett, C., 25-SDM-17 Messac, A., 2-MDO-1, 20-MDO-4, 40-MDO-7, 75MDO-10, 127-MDO-16 Michaeli, M., 45-SDM-30 Michalak, T., 103-SDM-70 Mignolet, M., 134-SDM-86 Miller, B., 46-SDM-31 Miller, D., 52-SDM-37 Millwater, H., 58-NDA-8, 112-NDA-12, 129-NDA-14, 133-SDM-85 Min, J., 66-SDM-45, 131-SDM-83 Mindelis, Y., 100-SDM-67 Minguet, P., 62-SDM-41, 113-SDM-72 Minisci, E., 128-NDA-13 Misra, A., 31-SDM-23 Missoum, S., 20-MDO-4, 75-MDO-10 Mital, S., 68-SDM-47 Modgil, G., 57-NDA-7 Moehring, M., 94-SDM-61 Moens, D., 86-SDM-59 Mohaghegh, M., 60-SDM-39 Mohan, R., 103-SDM-70 Mollenhauer, D., 62-SDM-41, 68-SDM-47 Mollineaux, M., 69-SDM-48 Moncada, A., 97-SDM-64 Monner, H., 54-ASC-2 Moody, J., 41-NDA-5 Moore, J., 108-GSF-6 Moore, K., 56-MDO-8 Morandini, M., 65-SDM-44 Mordasky, M., 121-SDM-80 Moreno, R., 27-SDM-19 Mori, O., 90-GSF-4 Morishima, R., 60-SDM-39 Morton, M., 63-SDM-42 Morton, S., 100-SDM-67 Moulin, B., 47-SDM-32 Muder, S., 130-SDM-82 Mukhopadhyay, V., 138-SDM-90 Mulani, S., 3-MDO-2, 63-SDM-42, 74-MDO-9, 91-MDO-11 Muraliraj, N., 62-SDM-41, 113-SDM-72 Murphey, T., 11-SDM-7, 23-SDM-15, 42-SDM-27, 131-SDM-83 Murphy, A., 6-SDM-2, 132-SDM-84 Murphy, D., 55-GSF-2, 90-GSF-4 Murphy, J., 34-SDM-26 Murua, J., 13-SDM-9, 30-SDM-22 Musil, E., 66-SDM-45 Na, Y., 28-SDM-20, 136-SDM-88 Naboulsi, S., 12-SDM-8 Nadella, K., 10-SDM-6 Nagappan, G., 116-SDM-75 Nagaraja, K., 135-SDM-87 Nagel, B., 126-MDO-15 Naik, N., 6-SDM-2 Naik, R., 86-SDM-59 Nair, A., 103-SDM-70 Najafi, A., 110-MDO-14, 128-NDA-13 Nakanishi, K., 125-GSF-8
Natarajan, B., 72-ASC-4 Natori, M., 55-GSF-2 Natterer, F., 92-MDO-12 Navaid, R., 57-NDA-7 Nay, J., 38-GSF-1 Nayfeh, A., 98-SDM-65, 104-SDM-71 Negoita, G., 40-MDO-7 Nelson, E., 62-SDM-41, 113-SDM-72 Nelson, J., 17-SDM-13 Neufeld, D., 20-MDO-4 Neuhart, R., 64-SDM-43 Newsom, J., 27-SDM-19 Ng, L., 111-NDA-11 Ngatu, G., 117-SDM-76 Nguyen, D., 98-SDM-65 Nguyen, H., 104-SDM-71 Nguyen, N., 98-SDM-65 Nguyen, S., 7-SDM-3 Ni, K., 9-SDM-5, 135-SDM-87 Nijssen, R., 52-SDM-37 Nikbay, M., 40-MDO-7, 99-SDM-66 Ning, S., 40-MDO-7 Ning, X., 101-SDM-68 Nishihara, T., 90-GSF-4 Nitzsche, F., 12-SDM-8, 29-SDM-21, 72-ASC-4, 82-SDM-55 Nogueira, A., 121-SDM-80 Nordin, P., 50-SDM-35 Noshadravan, A., 41-NDA-5 Nuhait, A., 69-SDM-48 O’Connor, A., 12-SDM-8 O’Donnell, M., 61-SDM-40 Ocampo, J., 112-NDA-12, 133-SDM-85 Ochinero, T., 8-SDM-4, 45-SDM-30 Odegard, G., 50-SDM-35, 85-SDM-58, 103-SDM-70 Oh, J., 41-NDA-5 Ohanian, O., 37-ASC-1 Ohara, C., 89-ASC-5 Ohayon, R., 119-SDM-78 Ohta, Y., 70-SDM-49 Ojha, S., 29-SDM-21 Okasinski, J., 15-SDM-11 Okuma, M., 108-GSF-6 Olave, M., 129-NDA-14 Olien, C., 37-ASC-1 Oliver, S., 96-SDM-63, 114-SDM-73 Olson, G., 108-GSF-6 Ondocsin, W., 96-SDM-63 Oremont, L., 114-SDM-73 Orr, A., 127-MDO-16
56
Orszulik, R., 55-GSF-2, 125-GSF-8 Ortega, D., 27-SDM-19 Oskay, C., 43-SDM-28 Oterkus, E., 44-SDM-29, 78-SDM-51, 130-SDM-82 Overmeyer, A., 29-SDM-21 Owens, S., 45-SDM-30 Owens, T., 97-SDM-64 Ozdemir Ozgumus, O., 66-SDM-45 Padget, J., 74-MDO-9 Padthe, A., 29-SDM-21 Padula, S., 91-MDO-11 Paez, T., 5-NDA-2, 22-NDA-4, 58-NDA-8, 129-NDA-14 Pahn, T., 87-SDM-60 Pai, P., 28-SDM-20, 59-SDM-38 Paiva, R., 56-MDO-8 Palacios, J., 29-SDM-21 Palacios, R., 13-SDM-9, 30-SDM-22, 130-SDM-82 Palazotto, A., 8-SDM-4 Palisoc, A., 73-GSF-3 Palmieri, F., 131-SDM-83 Pankow, M., 51-SDM-36 Paquet, J., 65-SDM-44 Paquette, J., 104-SDM-71 Park, C., 57-NDA-7 Park, G., 3-MDO-2, 70-SDM-49 Park, J., 130-SDM-82 Park, K., 118-SDM-77 Parks, G., 19-MDO-3 Parmigiani, J., 62-SDM-41 Parr, J., 127-MDO-16 Parsons, E., 50-SDM-35 Patel, D., 78-SDM-51, 95-SDM-62, 113-SDM-72 Patel, J., 57-NDA-7 Patil, M., 25-SDM-17, 65-SDM-44, 83-SDM-56, 84-SDM-57, 132-SDM-84 Pattabhiraman, S., 58-NDA-8 Patterson, K., 73-GSF-3 Paulson, E., 2-MDO-1, 57-NDA-7 Payette, S., 51-SDM-36 Peachey, T., 74-MDO-9 Pearson, J., 108-GSF-6 Peck, J., 63-SDM-42 Pedrotty, S., 42-SDM-27 Pellegrino, S., 73-GSF-3, 101-SDM-68, 108-GSF-6, 124-GSF-7 Pendleton, E., 19-MDO-3, 94-SDM-61 Peng, C., 11-SDM-7 Peng, H., 10-SDM-6 Peng, S., 79-SDM-52 Penmetsa, R., 58-NDA-8, 102-SDM-69
Peraza Hernandez, E., 30-SDM-22 Perry, B., 47-SDM-32 Perry, T., 81-SDM-54 Peters, G., 119-SDM-78 Peterson, M., 17-SDM-13 Petrolo, M., 78-SDM-51 Pettit, C., 69-SDM-48, 76-NDA-9 Phan, N., 9-SDM-5, 86-SDM-59 Philen, M., 37-ASC-1 Phillips, D., 96-SDM-63 Picard, G., 128-NDA-13 Picault, E., 131-SDM-83 Pickell, R., 113-SDM-72 Pineda, E., 43-SDM-28, 61-SDM-40 Pinho, S., 130-SDM-82 Pipes, B., 94-SDM-61 Pirmoradi, Z., 127-MDO-16 Pirrera, A., 33-SDM-25, 54-ASC-2 Pitt, D., 29-SDM-21, 63-SDM-42, 99-SDM-66 Pittman, C., 85-SDM-58, 103-SDM-70 Player, C., 38-GSF-1 Pleissner, M., 89-ASC-5 Pollayi, H., 10-SDM-6 Pontecorvo, M., 82-SDM-55 Pope, D., 117-SDM-76 Powell, D., 51-SDM-36, 122-SDM-81 Powell, E., 63-SDM-42 Prabhakar, P., 121-SDM-80 Price, M., 6-SDM-2 Probst, O., 17-SDM-13 Probst, T., 37-ASC-1 Provenza, A., 66-SDM-45 Prowell, I., 87-SDM-60, 104-SDM-71 Przekop, A., 23-SDM-15, 134-SDM-86 Puig, C., 51-SDM-36 Pun, A., 24-SDM-16 Purekar, A., 107-ASC-6 Quaranta, E., 84-SDM-57, 101-SDM-68 Quaranta, G., 65-SDM-44, 135-SDM-87 Quatmann, M., 132-SDM-84 Quilligan, A., 12-SDM-8 Quinn, D., 6-SDM-2, 132-SDM-84 Ragab, S., 129-NDA-14 Raghavan, S., 15-SDM-11 Raijmaekers, S., 52-SDM-37 Rais-Rohani, M., 39-MDO-6, 110-MDO-14, 128-NDA-13 Raju, G., 26-SDM-18 Raju, I., 79-SDM-52, 96-SDM-63 Ramnath, M., 62-SDM-41 Ranatunga, P., 25-SDM-17, 61-SDM-40
Author/Session Chair Index Rangavajhala, S., 75-MDO-10 Rankin, C., 23-SDM-15, 95-SDM-62, 114-SDM-73 Ransom, J., 21-NDA-3 Rassaian, M., 7-SDM-3 Raveendra, R., 45-SDM-30 Raveh, D., 13-SDM-9, 64-SDM-43 Ravichandran, K., 48-SDM-33 Ravishankar, B., 22-NDA-4 Rayburn, J., 131-SDM-83 Razak, N., 99-SDM-66 Reich, G., 37-ASC-1 Reimerdes, H., 132-SDM-84 Ren, J., 24-SDM-16 Ren, X., 32-SDM-24 Renaud, G., 79-SDM-52 Resor, B., 33-SDM-25 Rexius, S., 2-MDO-1 Reynolds, W., 42-SDM-27, 89-ASC-5, 107-ASC-6 Rhead, A., 26-SDM-18 Rhodes, O., 54-ASC-2 Rhymer, J., 7-SDM-3 Ricci, S., 49-SDM-34, 135-SDM-87 Ricciardi, A., 25-SDM-17, 83-SDM-56 Richards, J., 84-SDM-57 Richardson, T., 60-SDM-39 Ricks, T., 133-SDM-85 Riddick, J., 51-SDM-36 Riddle, T., 17-SDM-13 Riley, M., 93-NDA-10, 111-NDA-11 Riley, Z., 46-SDM-31 Rimoli, J., 43-SDM-28, 94-SDM-61 Risse, K., 74-MDO-9, 92-MDO-12 Ritter, M., 64-SDM-43 Ritz, E., 47-SDM-32 Rixen, D., 16-SDM-12 Rizzi, S., 134-SDM-86 Robbins, D., 62-SDM-41, 78-SDM-51, 113-SDM-72 Robertson, A., 87-SDM-60 Robertson, L., 30-SDM-22 Robinson, J., 91-MDO-11 Robinson, M., 24-SDM-16 Robinson, R., 38-GSF-1 Robinson, T., 127-MDO-16 Rodgers, T., 31-SDM-23 Rogers, G., 34-SDM-26 Rohl, P., 75-MDO-10, 109-MDO-13 Rojas, J., 43-SDM-28 Rolfes, R., 87-SDM-60, 114-SDM-73 Romanelli, G., 49-SDM-34, 138-SDM-90 Rome, J., 61-SDM-40, 78-SDM-51, 80-SDM-53, 95-SDM-62, 113-SDM-72 Romera, L., 60-SDM-39, 91-MDO-11 Romero, V., 5-NDA-2, 58-NDA-8 Ronzheimer, A., 92-MDO-12, 109-MDO-13 Rosario, S., 94-SDM-61 Rose, C., 77-SDM-50 Rose, T., 81-SDM-54 Ross, M., 5-NDA-2, 22-NDA-4, 135-SDM-87 Ross, R., 4-NDA-1 Rothkegel, J., 99-SDM-66 Roughen, K., 47-SDM-32 Rousseau, C., 45-SDM-30 Rowe, S., 120-SDM-79 Roy, A., 85-SDM-58, 103-SDM-70 Roy, S., 15-SDM-11, 31-SDM-23, 85-SDM-58, 102-SDM-69, 103-SDM-70 Runyon, B., 66-SDM-45 Ruzzene, M., 137-SDM-89 Saavedra Flores, E., 68-SDM-47, 123-ASC-7 Sabri, F., 81-SDM-54 Saether, E., 85-SDM-58 Saiz, A., 14-SDM-10 Sakamoto, H., 108-GSF-6 Salas, K., 10-SDM-6 Salehghaffari, S., 39-MDO-6 Samborsky, D., 52-SDM-37 Sanetrik, M., 47-SDM-32 Sangid, M., 31-SDM-23 Sankar, B., 128-NDA-13 Sankararaman, S., 5-NDA-2 Santer, M., 54-ASC-2, 73-GSF-3, 124-GSF-7 Sarhaddi, D., 49-SDM-34, 74-MDO-9, 104-SDM-71 Sarkar, S., 9-SDM-5, 86-SDM-59 Sas, P., 86-SDM-59 Satak, N., 30-SDM-22 Sathiskumar, A., 133-SDM-85 Satou, Y., 125-GSF-8 Saturni, A., 124-GSF-7 Satyanarayana, A., 62-SDM-41, 77-SDM-50 Savill, A., 2-MDO-1, 19-MDO-3, 74-MDO-9 Savvaris, A., 19-MDO-3 Sawada, H., 90-GSF-4 Saxon, J., 96-SDM-63 Scanlan, J., 84-SDM-57, 101-SDM-68 Schaub, H., 55-GSF-2 Scheider, K., 92-MDO-12 Schmauch, P., 12-SDM-8 Schonberg, W., 34-SDM-26 Schotte, J., 119-SDM-78
Schrell, J., 120-SDM-79 Schubel, P., 78-SDM-51, 95-SDM-62, 113-SDM-72 Schulte, K., 8-SDM-4 Schultz, M., 8-SDM-4, 45-SDM-30, 77-SDM-50, 114-SDM-73 Schumann, B., 84-SDM-57 Schutte, J., 120-SDM-79 Schwall, C., 94-SDM-61 Scott, M., 27-SDM-19 Scott, R., 47-SDM-32 Scott-Emuakpor, O., 66-SDM-45 Scotti, A., 134-SDM-86 Scotti, S., 4-NDA-1, 58-NDA-8, 80-SDM-53 Seaver, M., 97-SDM-64 Sebastiano, F., 135-SDM-87 Sedaghati, R., 107-ASC-6 Sehitoglu, H., 31-SDM-23 Seidel, G., 14-SDM-10, 32-SDM-24, 50-SDM-35, 68-SDM-47, 103-SDM-70, 121-SDM-80 Seiler, P., 20-MDO-4 Seltzer, A., 73-GSF-3 Senda, K., 125-GSF-8 Sensmeier, M., 113-SDM-72 Sepic Kriskovich, H., 99-SDM-66 Seshadri, P., 65-SDM-44 Seume, J., 70-SDM-49 Shah, R., 78-SDM-51 Shakib, F., 104-SDM-71 Shan, J., 55-GSF-2, 125-GSF-8 Shankar, R., 41-NDA-5 Shanmugam, V., 58-NDA-8 Shapiro, A., 122-SDM-81 Shapiro, E., 19-MDO-3 Shaw, L., 63-SDM-42 Shen, L., 27-SDM-19 Shi, F., 89-ASC-5 Shi, H., 24-SDM-16, 108-GSF-6 Shi, J., 14-SDM-10 Shimek, M., 34-SDM-26 Shimizu, Y., 92-MDO-12 Shimoda, M., 91-MDO-11 Shin, S., 28-SDM-20, 72-ASC-4, 136-SDM-88 Shirasawa, Y., 90-GSF-4 Shiryayev, O., 98-SDM-65, 116-SDM-75 Shivakumar, K., 7-SDM-3, 67-SDM-46 Shook, L., 108-GSF-6 Shousterman, A., 100-SDM-67 Shtark, A., 45-SDM-30 Sienz, J., 68-SDM-47 Sihn, S., 85-SDM-58
57
Sika, C., 7-SDM-3 Sikorski, R., 122-SDM-81 Silva, R., 83-SDM-56 Silva, W., 47-SDM-32 Silvernail, N., 70-SDM-49 Simard, B., 85-SDM-58 Simmermacher, T., 22-NDA-4 Simpson, T., 56-MDO-8 Simsiriwong, J., 86-SDM-59 Singh, G., 109-MDO-13, 129-NDA-14, 133-SDM-85 Singh, H., 117-SDM-76 Singh, K., 30-SDM-22 Sinha, S., 29-SDM-21, 34-SDM-26 Sinn, T., 38-GSF-1 Sivaneri, N., 116-SDM-75 Skujins, T., 81-SDM-54 Slater, J., 38-GSF-1, 116-SDM-75, 125-GSF-8, 136-SDM-88 Sleight, D., 131-SDM-83 Smarslok, B., 102-SDM-69 Smeltzer, S., 24-SDM-16, 94-SDM-61 Smith, A., 63-SDM-42, 66-SDM-45 Smith, E., 29-SDM-21, 94-SDM-61 Smith, M., 81-SDM-54 Smith, R., 77-SDM-50, 120-SDM-79 Smith, S., 85-SDM-58, 102-SDM-69, 136-SDM-88 Snyder, M., 25-SDM-17 Snyder, R., 65-SDM-44, 84-SDM-57 Socrate, S., 50-SDM-35 Sodano, H., 15-SDM-11 Sohn, Y., 15-SDM-11 Solcia, T., 138-SDM-90 Song, K., 96-SDM-63, 131-SDM-83 Soto, O., 117-SDM-76 Sotoudeh, Z., 83-SDM-56, 132-SDM-84 Soykasap, O., 108-GSF-6 Spall, J., 4-NDA-1 Spanrad, S., 86-SDM-59 Sparkman, D., 58-NDA-8 Spence, A., 49-SDM-34 Spiekermann, C., 100-SDM-67 Spottswood, S., 134-SDM-86 Sracic, M., 134-SDM-86 Srinivasan, G., 54-ASC-2 Stanfield, C., 95-SDM-62 Stanford, B., 3-MDO-2, 65-SDM-44, 127-MDO-16 Stanzl-Tschegg, S., 86-SDM-59 Stapleton, S., 24-SDM-16 Stargel, D., 102-SDM-69 Starkey, R., 57-NDA-7
Stavast, V., 23-SDM-15 Steckel, G., 78-SDM-51, 95-SDM-62, 113-SDM-72 Steeve, B., 96-SDM-63 Stelmack, M., 92-MDO-12 Stevens, W., 47-SDM-32 Stewart, E., 84-SDM-57 Stiles, L., 55-GSF-2 Stillinger, J., 31-SDM-23, 41-NDA-5 Stiltner, B., 37-ASC-1 Straubel, M., 55-GSF-2 Strganac, T., 104-SDM-71 Stromsoe, J., 80-SDM-53 Su, W., 82-SDM-55 Subbarayan, G., 41-NDA-5 Subramaniyan, A., 3-MDO-2, 22-NDA-4 Suleman, A., 56-MDO-8, 84-SDM-57 Sullivan, R., 86-SDM-59 Sung, H., 93-NDA-10 Surampudi, S., 13-SDM-9 Sutton, M., 109-MDO-13 Swanson, G., 96-SDM-63 Swenson, E., 97-SDM-64, 98-SDM-65 Swiler, L., 58-NDA-8 Swindeman, M., 62-SDM-41, 68-SDM-47 Söderberg, R., 101-SDM-68 Tabatabaei, Z., 122-SDM-81 Tackett, M., 110-MDO-14 Taft, B., 42-SDM-27 Taft, K., 42-SDM-27 Takahashi, K., 50-SDM-35 Takeda, K., 101-SDM-68 Tamilselvan, P., 97-SDM-64 Tamma, K., 137-SDM-89 Tandy, W., 73-GSF-3 Tarazaga, P., 55-GSF-2, 124-GSF-7 Tatman, J., 41-NDA-5 Taylor, P., 27-SDM-19, 49-SDM-34 Taylor, R., 9-SDM-5, 133-SDM-85 Templeton, J., 131-SDM-83 Teng, C., 67-SDM-46 Tessler, A., 80-SDM-53 Thacker, B., 5-NDA-2, 22-NDA-4 Thevamaran, R., 10-SDM-6 Thomas, G., 131-SDM-83 Thomas, M., 63-SDM-42 Thomsen, M., 138-SDM-90 Thomson, M., 108-GSF-6 Thormann, R., 83-SDM-56 Thornburgh, R., 29-SDM-21, 114-SDM-73 Tibbets, T., 73-GSF-3
Author/Session Chair Index Tibert, G., 38-GSF-1 Timme, S., 49-SDM-34, 112-NDA-12 Tippmann, J., 11-SDM-7 Tirey, B., 92-MDO-12 Tiwari, C., 94-SDM-61 Todoroki, A., 121-SDM-80 Toghiani, H., 85-SDM-58, 103-SDM-70 Tong, H., 63-SDM-42 Tong, J., 86-SDM-59 Tong, L., 123-ASC-7 Tonon, C., 51-SDM-36 Torng, T., 21-NDA-3, 93-NDA-10, 112-NDA-12 Toropov, V., 39-MDO-6, 127-MDO-16 Towner, R., 11-SDM-7, 63-SDM-42, 137-SDM-89 Trinh, K., 98-SDM-65 Triplett, M., 15-SDM-11 Tseng, C., 122-SDM-81 Tsuda, Y., 90-GSF-4 Tudor, A., 102-SDM-69 Tuegel, E., 4-NDA-1, 58-NDA-8, 102-SDM-69 Tutt, B., 38-GSF-1 Udwadia, F., 48-SDM-33 Ulker, F., 29-SDM-21 Urbina, A., 5-NDA-2, 22-NDA-4, 58-NDA-8 Ursache, N., 89-ASC-5 Uthandi, A., 133-SDM-85 Valdes, A., 118-SDM-77 Valdevit, L., 139-SDM-91 Valle, G., 124-GSF-7 Valverde, O., 95-SDM-62 Van Buren, K., 69-SDM-48 van der Laan, T., 101-SDM-68 van der Valk, P., 16-SDM-12 van Dijk, N., 3-MDO-2 van Dommelen, J., 92-MDO-12 Van Hooreweder, B., 86-SDM-59 Van Keulen, F., 3-MDO-2 van Schaik, J., 84-SDM-57 van Tooren, M., 109-MDO-13 Vanaerschot, A., 129-NDA-14 Vandepitte, D., 129-NDA-14 Vanhollebeke, F., 87-SDM-60 Vanneste, T., 65-SDM-44 Varshney, V., 85-SDM-58, 103-SDM-70 Vasconcellos, R., 98-SDM-65 Vasile, M., 38-GSF-1, 128-NDA-13 Vasista, S., 123-ASC-7 Vecherin, S., 76-NDA-9 Vedula, P., 82-SDM-55 Velazquez, E., 24-SDM-16, 97-SDM-64
Velicki, A., 94-SDM-61 Venkataraman, S., 57-NDA-7, 80-SDM-53 Venter, G., 4-NDA-1 Verbart, A., 3-MDO-2 Vescovini, R., 8-SDM-4 Viana, F., 20-MDO-4, 75-MDO-10, 111-NDA-11 Vieira, W., 72-ASC-4 Villanueva, D., 128-NDA-13 Vio, G., 25-SDM-17, 27-SDM-19, 95-SDM-62, 99-SDM-66 Viskanta, R., 122-SDM-81 Vocke, R., 72-ASC-4 Vogeler, K., 93-NDA-10 Voigt, M., 93-NDA-10 Volz, J., 122-SDM-81 von Reden, T., 120-SDM-79 Von Wahlde, R., 51-SDM-36 Vos, R., 92-MDO-12, 138-SDM-90 Voss, R., 83-SDM-56 Waas, A., 17-SDM-13, 24-SDM-16, 43-SDM-28, 45-SDM-30, 51-SDM-36, 61-SDM-40, 62-SDM-41, 80-SDM-53, 113-SDM-72, 121-SDM-80 Wadley, H., 31-SDM-23 Walker, S., 80-SDM-53 Walker, T., 62-SDM-41, 113-SDM-72 Wan, Z., 46-SDM-31, 138-SDM-90 Wang, G., 28-SDM-20, 56-MDO-8, 127-MDO-16 Wang, H., 80-SDM-53, 133-SDM-85 Wang, I., 100-SDM-67 Wang, J., 80-SDM-53, 113-SDM-72, 138-SDM-90 Wang, L., 22-NDA-4, 27-SDM-19 Wang, P., 70-SDM-49, 97-SDM-64, 128-NDA-13 Wang, Q., 54-ASC-2, 126-MDO-15 Wang, R., 109-MDO-13 Wang, Y., 48-SDM-33, 60-SDM-39 Wang, Z., 49-SDM-34, 98-SDM-65, 101-SDM-68, 104-SDM-71, 128-NDA-13 Wanthal, S., 44-SDM-29, 68-SDM-47, 121-SDM-80 Wardle, B., 8-SDM-4, 15-SDM-11, 50-SDM-35, 59-SDM-38, 85-SDM-58 Warren, J., 96-SDM-63 Waters, W., 77-SDM-50 Watson, L., 111-NDA-11, 136-SDM-88 Weaver, P., 8-SDM-4, 26-SDM-18, 33-SDM-25, 54-ASC-2, 61-SDM-40, 72-ASC-4, 115-SDM-74 Weckner, O., 39-MDO-6, 62-SDM-41 Wei, J., 139-SDM-91 Weisshaar, T., 25-SDM-17 Wellman, G., 5-NDA-2 Welsh, W., 66-SDM-45
Wereley, N., 38-GSF-1, 72-ASC-4, 117-SDM-76 Whitcomb, J., 32-SDM-24 White, C., 11-SDM-7 Whiting, B., 64-SDM-43 Wickramasinghe, V., 29-SDM-21, 48-SDM-33 Wicks, S., 50-SDM-35 Widana-Gamage, D., 54-ASC-2 Widener, C., 66-SDM-45 Wiedemann, M., 55-GSF-2 Wiegand, D., 21-NDA-3 Wieseman, C., 13-SDM-9, 47-SDM-32 Wijnands, Q., 128-NDA-13 Wilbur, M., 29-SDM-21 Wilhite, A., 2-MDO-1 Wilkie, K., 89-ASC-5, 90-GSF-4 Willcox, K., 20-MDO-4, 56-MDO-8 Willey, C., 38-GSF-1 Williams, A., 42-SDM-27 Williams, M., 50-SDM-35 Williams, T., 59-SDM-38 Williamsen, J., 34-SDM-26 Willis, B., 59-SDM-38, 118-SDM-77 Wilson, D., 76-NDA-9 Wilson, T., 138-SDM-90 Wilt, D., 131-SDM-83 Winer, E., 40-MDO-7 Wingate, R., 96-SDM-63 Witteveen, J., 76-NDA-9, 111-NDA-11 Wittmann, J., 89-ASC-5 Wolfe, K., 44-SDM-29 Wolff, M., 80-SDM-53 Woo, K., 17-SDM-13, 73-GSF-3, 125-GSF-8 Woolsey, C., 84-SDM-57 Workman, J., 17-SDM-13 Worotynska, J., 95-SDM-62 Wright, T., 62-SDM-41 Wu, J., 2-MDO-1 Wu, M., 49-SDM-34 Wu, W., 41-NDA-5 Wu, Z., 26-SDM-18, 27-SDM-19 Xiang, Y., 102-SDM-69 Xie, C., 25-SDM-17 Xie, J., 37-ASC-1 Xu, J., 19-MDO-3, 40-MDO-7, 68-SDM-47, 86-SDM-59 Yabili, S., 81-SDM-54 Yagoubi, J., 122-SDM-81 Yamakawa, H., 55-GSF-2 Yamamoto, N., 10-SDM-6 Yamazaki, W., 127-MDO-16 Yang, B., 108-GSF-6, 124-GSF-7
58
Yang, C., 25-SDM-17, 27-SDM-19, 120-SDM-79 Yang, J., 95-SDM-62, 109-MDO-13 Yang, M., 95-SDM-62 Yang, S., 16-SDM-12, 103-SDM-70, 109-MDO-13 Yang, Y., 104-SDM-71 Yang, Z., 37-ASC-1 Yarrington, P., 45-SDM-30 Yavuzbalkan, E., 28-SDM-20 Ydrefors, L., 50-SDM-35 Ye, Z., 139-SDM-91 Yekani Fard, M., 97-SDM-64, 133-SDM-85 Yen, C., 51-SDM-36 Yerramalli, C., 17-SDM-13 Yokoyama, J., 125-GSF-8 Yoo, J., 107-ASC-6 Yoon, H., 107-ASC-6 York, C., 6-SDM-2, 25-SDM-17 Youn, B., 21-NDA-3, 70-SDM-49, 107-ASC-6 Yu, J., 103-SDM-70 Yu, S., 103-SDM-70 Yu, W., 10-SDM-6, 33-SDM-25, 49-SDM-34, 54-ASC-2, 67-SDM-46, 86-SDM-59, 122-SDM-81, 139-SDM-91 Zander, M., 131-SDM-83 Zhan, K., 24-SDM-16 Zhang, C., 68-SDM-47 Zhang, J., 2-MDO-1, 20-MDO-4, 40-MDO-7, 44-SDM29, 75-MDO-10, 127-MDO-16 Zhang, W., 95-SDM-62 Zhang, X., 24-SDM-16, 79-SDM-52 Zhang, Z., 49-SDM-34 Zhao, H., 31-SDM-23 Zhou, E., 68-SDM-47 Zhu, C., 137-SDM-89 Zhu, Z., 109-MDO-13 Zhupanska, O., 8-SDM-4 Zimcik, D., 29-SDM-21 Zipay, J., 95-SDM-62, 132-SDM-84 Zongren, W., 95-SDM-62 Zuo, Q., 10-SDM-6
Author/Session Chair Index
