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This calculator computes the displacement of a simply-supported circular plate under a uniformly distributed load.

Inputs
Loading:	Uniform load p =   Pa kPa MPa GPa psi ksi lbf/ft^2 kgf/cm^2 atm bar mmHg inHg ftH2O
Geometry:	Radius ro =     km m cm mm micron mi yd ft in mil  Thickness h =     km m cm mm micron mi yd ft in mil
Material:	Young's modulus E =     Pa kPa MPa GPa psi ksi lbf/ft^2 kgf/cm^2 atm bar mmHg inHg ftH2O  Poisson's ratio =
Output:	Unit of displacement w =   km m cm mm micron mi yd ft in mil  Unit of stress =   Pa kPa MPa GPa psi ksi lbf/ft^2 kgf/cm^2 atm bar mmHg inHg ftH2O

Notice that the deformation is axial symmetric and it is only a function of the radius.

Hence, = 0.271728515625 mm 0.272 mm

The maximum bending moment occurs at the center of the plate, r = 0.

The maximum stress occurs at the center of the plate near surface, r = 0, z = ±h/2.

_max = 0.7734375 MPa 0.773 MPa