Page 363 - Modelling in Transport Phenomena A Conceptual Approach
P. 363

9.2.  ENERGY TRANSPORT WITHOUT CONVECTION                           343


              Since T  = T(z), Table C.4 in  Appendix  C indicates that  the only  non-zero
           energy flux component is e,  and it is given by

                                                                            (9.2-2)

           For  a rectangular volume element of  thickness AZ as shown in  Figure 9.5,  Eq.
           (9.2-1) is expressed as
                                qZl,  A - qzIr+Ar A +   AZ = 0              (9.2-3)

          Dividing each term by AAz and taking the limit as AZ ---f 0 gives

                                                                            (9.2-4)

          or
                                          -- - g                            (9.2-5)
                                          dqz
                                           dz
           Substitution of Eq.  (9.2-2) into &.  (9.2-5) gives the governing equation for tem-
          perature 8s
                                                                            (9.2-6)

          Integration of  Eq.  (9.2-6) gives


                                                                            (9.2-7)

          where u is  a  dummy variable of integration and C1 is  an integration constant.
          Integration of  Eq.  (9.2-7) once more leads to


                        l'k(T) dT = - 1' [I' X(u) d] dz + CI + C2           (9.2-8)
                                                              z

          Evaluation of  the constants Cl and C2 requires the boundary conditions to  be
          specified. The solution of h. (9.28) will be presented for two types of  boundary
          conditions, namely, Type I and Type 11. In the case of  Type I boundary condi-
          tion, the temperatures at both surfaces are specified. On the other hand, Type I1
          boundary condition implies that while the temperature is specified at one of  the
          surfaces, the other surface is subjected to a constant wall heat flux.

          Type I boundary condition
          The solution of Eq.  (9.2-8) subject to the boundary conditions

                                    at  z=O      T=T,
                                                                            (9.2-9)
                                    at  z=L      T=TL
   358   359   360   361   362   363   364   365   366   367   368