Objective

To determine the maximum displacements and bending moments in a square plate simply supported along the perimeter and subjected to a uniformly distributed load p.

Reference

Strength, stability, and vibrations. Handbook in Three Volumes. Volume 1. Edited by I.A.Birger and Y.G.Panovko. — M.: Mashinostroyenie, 1968, pp. 532-535.

Problem statement

A square isotropic plate of constant thickness is simply supported along its perimeter and subjected to a uniformly distributed load p.

To determine: the maximum displacements and the maximum bending moments.

Design model

The design model is a beam grillage, slab.

Initial geometry

Initial geometry

Geometry

Slab side dimension a = 1,5 m
Plate thickness h = 0,01 m

Material properties

Modulus of elasticity Е = 2,0 * 108 kPa
Poisson's ratio ν = 0,3

Boundary conditions

Hinged support of nodes along the contour out of the XOY plane (displacement w = 0).

Restraints are applied in the X, Y, and uZ degrees of freedom directions at the centre of the plate.

Loads

Load p = 10 kPa

Output data

Design model Displacements w, mm
Design model
Displacements w, mm
Bending moments Mx, kN*m/m Bending moments My, kN*m/m
Bending moments Mx, kN*m/m
Bending moments My, kN*m/m

Analytical solution

In the analytical solution, the displacement w and the bending moments Mx and My at the centre of the plate are calculated using the following formulas:

w = 0,00406*(p*a4)/D, where
D = (E*h3)/(12*(1-ν));
Mx = My = 0,0479*p*a2.

Comparison of calculation results

Parameter Theory LIRA-FEM Error, %
Displacement at plate centre w, mm -11,22 -11,23 0,09
Bending moment Mx, kN*m/m 1,078 1,065 1,2
Bending moment My, kN*m/m 1,078 1,065 1,2

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