2D Steady State Temperature Distribution Matrix Structural Analysis
Giuliano Basile Vinh Nguyen Christine Rohr University of Massachusetts Dartmouth
July 21, 2010
Introduction Advisor Dr. Nima Rahbar: Civil Engineer
Project Description Learning the fundamentals for creating matrices. We will be working with 2 Dimensional frames. Constructing elements and nodes, which will be used to study temperature distribution through out our specimen.
Application of Research Study the thermal distribution Test different types of materials Compare Numerical vs. Analytical results Basile, Nguyen, Rohr (UMD)
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Objectives
Use Matlab to calculate the 2D Steady State Temperature Distribution Consider the boundary conditions (will be discussed) Use Triangular Elements Compare your numerical solution with the exact analytical solution Calculate number of nodes, elements needed for accurate results Compute Errors
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Thermal Distribution in Materials
We consider all materials to be at Steady State Different materials have different temperature distributions; This is due to different atomic structures Metals – Crystalline Ceramics – Amorphous Polymers – Chains
Atomic structure leads to different Thermal Conductivity (how heat travels throughout)
This knowledge can be to choose the correct material for engineering designs
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Metals
Figure: Crystalline Atomic Structure
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Ceramics
Figure: Amorphous Atomic Structure Basile, Nguyen, Rohr (UMD)
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Polymers
Figure: Chain Atomic Structure
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Thermal Distribution in Materials Table: Thermal Conductivity of Materials (Watts/meter*Kelvin)
Basile, Nguyen, Rohr (UMD)
Materials
Values
Wood Rubber Polypropylene Cement Glass Soil Steel Lead Aluminum Gold Silver Diamond
0.04-0.4 0.16 0.25 0.29 1.1 1.5 12.11-45.0 35.3 237.0 318.0 429.0 90.0-2320.0
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Why study 2D Thermal Distribution?
To generate new understanding and improve computer methods for calculating thermal distribution. 2D computer modeling is cheap fast to process gives accurate numerical results parallel method can be used for higher efficiency
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Short Description Here we are modeling heat flux for a 2D plate No heat is applied to the x and y axis (x-nodes = y-nodes = 0) Flux is also considered zero on the right side of the plate Steady heat is being applied at the top of the plate: θ = 100 sin(
πx ) 10
(1)
! Basile, Nguyen, Rohr (UMD)
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What’s Included Elements We start with 32 triangular elements Numbering left to right; bottom to top Each element has 3 local and global nodes Number of Elements and Global Nodes will change
Nodes Local nodes are used to indicate Global nodes Nodes are used to define elements Independent Element Number ien (3,5) = 17 3 is the Local node number 5 is the Element number 17 is the Global node number Basile, Nguyen, Rohr (UMD)
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25 Nodes (32 Elements) — Plate vs. MatLab Solution Temperature Distribution
10
90
9
85
8
80
Vertical Side
7
75
6
70
5
65
4 60 3 55 2 50 1 45 0
0
1
2 3 4 Horizontal Side
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81 Nodes (128 Elements) — Plate vs. MatLab Solution Temperature Distribution
10 9
90 8
Vertical side
7
85
6 5
80
4 75
3 2
70
1 0
0
1
2 3 4 Horizontal side
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324 Nodes (512 Elements) — Plate vs. MatLab Solution Temperature Distribution
10
96 9 94
8
Vertical side
7
92
6 90 5 88
4 3
86
2 84 1 0
82 0
1
2 3 4 Horizontal side
5
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900 Nodes (1682 Elements) — Plate vs. MatLab Solution Temperature Distribution
10
98
9 97 8 96
Vertical Side
7 95
6 5
94
4
93
3
92
2 91 1 90 0
0
1
2 3 4 Horizontal Side
5
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Temperature Distribution (Right Side) 100 sinh πy 10 sin δ(x, y ) = sinh(π)
πx 10
100 90 80
Temperature
70 60
32 Elements
50 40 30 20 10 0
0
1
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3
4
5 Y!Axis
6
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7
8
9
10
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Temperature Distribution (Right Side) 100 sinh πy 10 sin δ(x, y ) = sinh(π)
πx 10
100 90 80
Temperature
70 60 50
128 elements
40 30
32 elements
20 10 0
0
1
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3
4
5 Y!Axis
6
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7
8
9
10
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Temperature Distribution (Right Side) 100 sinh πy 10 sin δ(x, y ) = sinh(π)
πx 10
100 90 80
Temperature
70
128 elements
60 50
32 elements
40 30
512 elements
20 10 0
0
1
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3
4
5 Y!Axis
6
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7
8
9
10
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Temperature Distribution (Right Side) 100 sinh πy 10 sin δ(x, y ) = sinh(π)
πx 10
100
Temperature at The Right Side of The Plate
90 80
Temperature
70 60 50 The temperature lines converge to a smooth line as the number of elements increases
40 30
32 elements 128 elements 512 elements 1682 elements
20 10 0
0
1
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3
4
5 Y!Axis
6
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8
9
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Maximum Error Computed 32 elements
7
128 elements
2
5
Percentage Error
Percentage Error
6
4 3 2
1.5
1
0.5
1 0
0
1
2
3
4
0
5
0
1
2
X!axis
512 elements
0.45
3
4
5
4
5
X!axis
1682 elements
0.14
0.4
0.12 Percentage Error
Percentage Error
0.35 0.3 0.25 0.2 0.15
0.1 0.08 0.06 0.04
0.1 0.02
0.05 0
0
1
2
3
4
5
0
0
X!axis
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2
3 X!axis
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What’s Next???
Goals Continue modeling temperature change Add defect to material and relate it to original material Add hole to the specimen to be continued...
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References [Civil Engineer] Dr. Nima Rahbar Fundamental Matrix Algebra University of Massachusetts Dartmouth, Summer 2010. [Thermal Conductivity of some common Materials] Thermal Conductivity of Materials www. engineeringtoolbox. com , July 2010 Cu Atomic Structure Crystalline Atomic Structure http: // www. webelements. com , July 2010 Ceramic Atomic Structure Amorphous Atomic Structure http: // www. bccms. uni-bremen. de , July 2010 Polymer Atomic Structure Chain Atomic Structure http: // www. themolecularuniverse. com , July 2010
Thank You for Listening We would like to take this time to thank some very special people during this whole learning process. Dr. Gottlieb Dr. Davis Dr. Kim Dr. Rahbar Dr. Hausknecht CSUMS Staff Daniel Higgs Zachary Grant Charels Poole Sidafa Conde CSUMS Students
Questions?
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