Page 62 - Mechanics Analysis Composite Materials
P. 62

Chapter 2.  Fundamentals of mechunics of solids   47
            Symmetry conditions.  Eqs. (2.50),  reduce to




            These  equations  have  a  simple  physical  meaning.  The  higher  the  stiffness  is,
            demonstrated by the material in some direction, the less is the strain in this direction
            under  loading  in  the  orthogonal  directions.  Taking  into  account  the  foregoing
            symmetry conditions we can conclude that an orthotropic material is characterized
           with nine independent elastic constants.
             The  simplest  material  model  corresponds  to  the  isotropic  material,  whose
           mechanical  properties  are the  same for  any direction  or  plane  of  loading.  As  a
            result,  subscripts  indicating coordinate  directions  and planes  in  Eq. (2.53) disap-
           pear, and it reduces to

                       I     1'   1'
                       -   _-   __   0   0  0
                       E     E    E


                             v
                      __  __     I   0   0  0
                        1'
                        E    E   E
               [CI =                  I                                      (2.54)
                       0    0    0   -  0  0
                                     G
                                         1
                       0    0    0   0-0
                                         G
                                            1
                       0    0    0   00-
                                            G
           Compliance  matrix,  Eq. (2.54),  contains  three  elastic  constants,  E,  G,  and  Y.
            However, only two of  them are independent. To show this, consider the problem
           of pure shear for a plate discussed in Section 2.4 (see Fig. 2.5). For this problem,
           cr,  = cr,  = cr,  = z,   = zIz = 0,z,,  = z and Eqs. (2.48) and (2.54) yield




           Specific strain energy in 33q. (2.51) can be written as





            However,  as follows from  Section 2.4, pure shear can  be  reduced  to tension  and
           compression  in  the  principal  directions  (see  Fig. 2.5).  For  these  directions,
            Eqs. (2.48) and (2.54) give
   57   58   59   60   61   62   63   64   65   66   67