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82                           Chapter 5  Plate Bending analysis



                              an application example at the end of the chapter to demonstrate the
                              advantages of the finite element method.


                              5.1   Basic Equations

                                  5.1.1  Differential Equation
                                         Derivation of the differential equation for plate bending
                              is similar to that for the beam bending as explained in Chapter 3.  A
                              thin plate with its thickness of  h that lies in the x-y plane is shown
                              in the figure.  The plate is subjected to the pressure of  (, )p x y  on
                              the upper surface causing the deflection of w in the z-direction and
                              the  in-plane  displacement  of  u  and  v in  the  x-  and  y-direction,
                              respectively.

                                                            xy
                                                          p (, )

                                                               u
                                                                                 x

                                                     v      w




                                             y                    h
                                                          z

                                         The  basic  assumption  of  plane  section  remains  plane
                                                                                    z w x
                              before and after deflection leads to the relations of  u    
                              and  v  z w y .  Together with the additional assumption of the
                                         
                                            
                              deflection  w  that  varies  with  x  and  y  only,  w   w (, ) ,  the
                                                                                  x
                                                                                     y
                              governing differential equation representing equilibrium condition
                              of plate bending can be derived in the form,
                                              M x    2    2 2  M xy      2  M y       
                                                                             p
                                              x   2    xy     y   2

                              where the bending moment components are,
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