Page 112 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
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STEADY STATE HEAT CONDUCTION IN ONE DIMENSION
                        104

                                            q a  T 1    T 2  T 3  T 4
                                                                          h, T a








                                                    x 1   x 2  x 3
                                        Figure 4.2 Heat conduction in a composite wall

                           Rearranging, we obtain

                                                      Q
                                                         =−(T 2 − T 1 )
                                                     k 1 A
                                                      x 1
                                                      Q
                                                     k 2 A  =−(T 3 − T 2 )

                                                      x 2
                                                      Q
                                                         =−(T 4 − T 3 )                      (4.8)
                                                     k 3 A
                                                      x 3
                           Adding the above equations and rearranging,
                                                           (T 1 − T 4 )
                                                                                             (4.9)
                                                 Q =
                                                        x 1   x 2   x 3
                                                           +     +
                                                       k 1 A  k 2 A  k 3 A
                           The numerator in the above equation is often referred to as the thermal potential differ-
                        ence and the denominator is known as the thermal resistance. In general, all x/kA terms
                        are called thermal resistances (See Figure 4.2). If there is a convective resistance, say on
                        the right face, then we have (Q = hA(T 4 − T a )).

                                                           (T 1 − T a )
                                               Q =                                          (4.10)
                                                     x 1   x 2   x 3   1
                                                        +     +     +
                                                    k 1 A  k 2 A  k 3 A  hA
                        where h is the heat transfer coefficient from the right wall surface to the atmosphere
                        and T a is the atmospheric temperature. Let us now consider a finite element solution
                        for Equation 4.1. As shown in Equation 4.6, the temperature distribution is linear for a
                        homogeneous material.
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