FixPlate

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fixplate04

{ FIXPLATE.PDE

   ***********************************************

 

   This example considers the bending of a thin rectangular plate under a

   distributed transverse load.

 

   For small displacements, the deflection U is described by the Biharmonic

   equation of plate flexure

 

       del2(del2(U)) + Q/D  =  0

 

   where

       Q is the load distribution,

       D = E*h^3/(12*(1-nu^2))

       E is Young's Modulus

       nu is Poisson's ratio

   and h is the plate thickness.

 

   The boundary conditions to be imposed depend on the way in which the

   plate is mounted.  Here we consider the case of a clamped boundary,

   for which

 

       U = 0

       dU/dn = 0

 

   FlexPDE cannot directly solve the fourth order equation, but if we

   define V = del2(U), then the deflection equation becomes

 

       del2(U) = V

       del2(V) + Q = 0

 

   with the boundary conditions

 

       dU/dn = 0

       dV/dn = L*U

 

   where L is a very large number.

 

   In this system, dV/dn can only remain bounded if U -> 0, satisfying the

   value condition on U.

 

   The particular problem addressed here is a plate of 16-gauge steel,

   8 x 11.2 inches, covering a vacuum chamber, with atmospheric pressure

   loading the plate.  The edges are clamped.  Solutions to this problem

   are readily available, for example in Roark's Formulas for Stress & Strain,

   from which the maximum deflection is Umax =  0.219, in exact agreement

   with the FlexPDE result.

 

   (See FREEPLATE.PDE for the solution with a simply supported edge.)

 

   Note: Care must be exercised when extending this formulation to more complex

   problems.  In particular, in the equation del2(U) = V, V acts as a source

   in the boundary-value equation for U.  Imposing a value boundary condition

   on U does not enforce V = del2(U).

 

   }

 

 

title " Plate Bending - clamped boundary "

 

Select

   errlim = 0.005

   cubic                { Use Cubic Basis }

 

Variables

    U(0.1)

    V(0.1)

 

Definitions

   xslab = 11.2

   yslab = 8

   h = 0.0598  {16 ga}

   L = 1.0e4

   E = 29e6

   Q = 14.7

   nu = .3

   D = E*h**3/(12*(1-nu**2))

 

Initial values

   U =  0

   V =  0

 

Equations

    U:        del2(U) = V

    V:        del2(V) = Q/D

 

Boundaries

   Region 1

     start (0,0)

     natural(U) = 0

     natural(V) = L*U

     line to (xslab,0)

          to (xslab,yslab)

          to (0,yslab)

          to close

 

monitors

   contour(U)

 

plots

   contour (U)  as "Displacement"

   elevation(U) from (0,yslab/2) to (xslab,yslab/2) as "Displacement"

   surface(U) as "Displacement"

 

end