Research Article

Applicable Formulas for Shear and Thermal Buckling of Perforated Rectangular Panels

Table 3

Normalized buckling loads for square (a/b = 1.0) simply supported (SSSS) perforated panel exposed to shear load case.

d/bSFSM [3]FEM [3]Pham equations [3]Reference [4]FEM [4]Present equation (2)

09.3289.3289.3289.2359.249.340
0.059.0599.1258.9978.893
0.18.4878.5628.478.6838.4798.306
0.157.7377.7977.7477.625
0.26.9386.9986.8287.0546.9486.895
0.256.1536.1996.1226.157
0.35.4095.4455.3825.4655.4035.440
0.354.7184.7534.7044.768
0.44.094.1214.0864.0894.0514.153
0.453.533.5563.5283.601
0.53.0383.0593.0322.9982.9693.113
0.552.6122.6292.5962.687
0.62.2472.252.2392.1852.1622.318
0.651.9361.941.9591.999
0.71.6721.6761.6791.726
0.751.4491.4461.3991.493
0.81.261.2511.1191.293