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9.1 Basic Equations                                       167



                                     9.1.2  Related Equations
                                           The  governing  differential  equations  in  the  preceding
                                 section are derived by using the Fourier’s law.  The law relates the
                                 conduction  heat  flux  components  with  the  temperature  gradients.
                                 For isotropic material, the conduction heat flux in the x-direction is,
                                                                     T
                                                         q      k
                                                          x
                                                                     x 
                                            Boundary  conditions  of  heat  transfer  at  the  domain
                                 surface may consist of,
                                      (a)  Specified temperature,

                                                            T    T
                                                                  s
                                 where T  may be constant or varies with x-, y-, z-coordinates and
                                        s
                                 time t.
                                      (b)  Specified heat flux,

                                                              q   q

                                                                   s
                                 where  q  is the specified heat flux which must be in equilibrium
                                         s
                                 with the conduction heat flux q at the surface.
                                       (c)  Convection heat transfer,
                                                         q   (T  T  )
                                                             h
                                                                s
                                 where  h is  the  surface  convection  coefficient  and T  is  the
                                                                                      
                                 surrounding medium temperature.
                                       (d)  Radiation heat transfer,

                                                              q   ( T   4  )T
                                                                 4
                                                                 s   
                                 where   is the surface emissivity and    is the Stefan-Boltzmann
                                 constant.
                                            For  transient  heat  transfer,  an  initial  condition  is
                                 needed,
                                                    Tx   y  z     T 0  x  y  z
                                                      (, , ,0)    ( , , )
                                 where T  is the initial temperature of the solid.
                                        0
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