Consider the triangular panel made of two different isotropic materials as shown in Fig. 2. A constant temperature of T = 0°C is prescribed along edge 2–3. Edge 1–2 is fully insulated. A linearly-varying heat flux of q = 15x W m-1 is applied along edge 1-3. Heat sources can be ignored. The panel is approximated using two linear triangular elements as indicated in Fig. 2. 2 (1) (1) q = 0 T = 0°C 3 m N(1) N(2) k = 4W°C-1 |k = 8 W °C-1 (2) (3) (2) 3 -1 q = 15x W m' 2 m 2 m Figure 2: Bi-material triangular panel. (a) Compute the element conductance matrix Ke for element 1. (b) Compute the global flux vector f. (c) Compute the global conductance matrix after imposition of the essential bound- ary conditions.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
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Chapter2: Steady Heat Conduction
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Q3
Consider the triangular panel made of two different isotropic materials as shown in
Fig. 2. A constant temperature of T = 0°C is prescribed along edge 2-3. Edge 1–2 is
fully insulated. A linearly-varying heat flux of ą
= 15x W m-1 is applied along edge
1-3.
Heat sources can be ignored.
The panel is approximated using two linear triangular elements as indicated in Fig. 2.
2
(1) (1)
q = 0
T = 0°C
3 m
N(1)
N(2)
k = 4W°C-1 |k = 8 W°C-1
(3) (2)
(2)
(3)
4
3
-1
q = 15x W m
2 m
2 m
Figure 2: Bi-material triangular panel.
(a) Compute the element conductance matrix Kº for element 1.
(b) Compute the global flux vector f.
(c) Compute the global conductance matrix after imposition of the essential bound-
ary conditions.
Page 4 of 6
Continued overleaf
Transcribed Image Text:Q3 Consider the triangular panel made of two different isotropic materials as shown in Fig. 2. A constant temperature of T = 0°C is prescribed along edge 2-3. Edge 1–2 is fully insulated. A linearly-varying heat flux of ą = 15x W m-1 is applied along edge 1-3. Heat sources can be ignored. The panel is approximated using two linear triangular elements as indicated in Fig. 2. 2 (1) (1) q = 0 T = 0°C 3 m N(1) N(2) k = 4W°C-1 |k = 8 W°C-1 (3) (2) (2) (3) 4 3 -1 q = 15x W m 2 m 2 m Figure 2: Bi-material triangular panel. (a) Compute the element conductance matrix Kº for element 1. (b) Compute the global flux vector f. (c) Compute the global conductance matrix after imposition of the essential bound- ary conditions. Page 4 of 6 Continued overleaf
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