Page 163 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
P. 163

TRANSIENT HEAT CONDUCTION ANALYSIS
                                                  i   Cross-sectional area, A  j              155
                                                            l

                                                             x


                                          Figure 6.2 One-dimensional linear element

                           The temperature T is represented in the element by

                                                 T = N i T i + N j T j = [N]{T}             (6.24)

                           Note that i and j in the above equation represent the nodes i and j of the element
                        shown in Figure 6.2. The shape functions in Equation 6.24 are defined as

                                                                x
                                                        N i = 1 −
                                                                l
                                                             x
                                                       N j =                                (6.25)
                                                             l
                           The spatial derivative of temperature is given as
                                        ∂T    ∂N i    ∂N j      1     1
                                            =    T i +   T j =− T i + T j = [B]{T}          (6.26)
                                        ∂x    ∂x      ∂x        l     l
                           The relevant matrices, as discussed in the previous section (Equation 6.16), are

                                                                        2
                                                    T                 N i  N i N j
                                      [C] =   ρc p [N] [N]d
 =  ρc p A        2  dl         (6.27)
                                             
                l      N i N j  N j
                           Note that d
 is replaced by Adl in the above equation. Here, A is the uniform cross-
                        sectional area of a one-dimensional body. The integration of Equation 6.27 results in (for
                        details of the integration, refer to Chapter 3 and Appendix B)


                                                          ρc p lA 21
                                                    [C] =                                   (6.28)
                                                            6   12
                           Similarly, the [K] matrix and load vector {f} can be written as

                                                   Ak x   1 −1    hP l 21
                                             [K] =              +                           (6.29)
                                                    l   −1   1     6   12
                        and


                                                GAl 1     qP l 1    hT a Pl 1
                                           {f}=         −         +                         (6.30)
                                                 2   1      2   1      2   1
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