For the following calculations we will only consider plates of uniform thickness and with a uniformly distributed load over the entire surface. This will help us define minimum thickness’ for components such as pressure vessels or piston housings.

Simply Supported

The maximum bending stress of a simply supported plate can be calculated by:

Stress at centre of plate

a=plate length, b=plate width

B=constant (see table) q=load per unit area, b=plate width, t=plate thickness
a/b1.01.21.41.61.82.03.04.05.0
0.28740.37620.45300.51720.56880.61020.71340.74100.74760.7500

For values of a/b not given in table, round down to the next respective value i.e. assuming maximum stress values for conservatism.

Fixed Support

For a plate that is fixed supported i.e. built into the structure, the maximum bending stress (at the centre of longer edges) can be calculated by:

Max stress at centre of long edge

B=constant (see table B) q=load per unit area, b=plate width, t=plate thickness

Stress at centre of plate

B=constant (see table B) q=load per unit area, b=plate width, t=plate thickness
a/b1.01.21.41.61.82.0
0.30780.38340.43560.46800.48720.49740.5000
0.13860.17940.20940.22860.24060.24720.2500

For values of a/b not given in table, round down to the next respective value i.e. assuming maximum stress values for conservatism.


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