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10.1 Basic Equations                                      187



                                            These  six  stress  components  depend  on  the  six  strain
                                 components and temperature.  The six strain components are func-
                                 tions  of  the  three  displacement  components  ,u   ,v   w  in  the  ,x   ,y

                                 z  directions, respectively.  The three displacement components are
                                 solved from the three governing differential equations above.

                                     10.1.2  Related Equations

                                            Boundary conditions for heat transfer problem are: (a)
                                 specified  temperature,  (b)  specified  surface  heating,  (c)  surface
                                 convection,  and  (4)  surface  radiation.    Details  of  these  boundary
                                 conditions are provided in chapter 9.
                                            Boundary  conditions  for  stress  analysis  of  solid  pro-
                                 blem are: (a) specified displacements, and (b) specified tractions on
                                 the  solid  surface.    Details  of  these  boundary  conditions  are
                                 described in chapter 6.
                                            The basic unknowns of the solid problem are the three
                                 displacement components  ,u   ,v   w  which are solved from the three
                                 governing  differential  equations.    Since  the  differential  equations
                                 are written in forms of the stress components, the relations between
                                 the stress and displacement components must be provided.
                                            The six stress components can be written in forms of
                                 the six strain components as,
                                                       
                                                                  0 
                                                                C
                                                       
                                                                
                                                                      
                                                      (6 1)    (6 6)  (6 1)
                                                     T
                                                   
                                 where                         xy   xz   
                                                                              yz 
                                                          
                                                             x
                                                                    z
                                                                y
                                             C
                                 The  matrix   is  the  material  elasticity  matrix.    The  total  and
                                 thermal strain components are,
                                                  T       xy   xz   
                                                        
                                                                           yz 
                                                          x
                                                                z
                                                             y
                                                 T           T      T     T  000  
                                                
                                                 0
                                                                                     
                                 where    is  the  coefficient  of  thermal  expansion  and  T  is  the
                                 difference between the temperature and reference temperature T
                                                                                            ref
                                 for zero stress,
                                                      T    T (, , )   x  y  z  T ref
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