Modelling and Simulation in Engineering / 2012 / Article / Tab 3

Research Article

Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression

Table 3

The formulas for predicting the buckling load reduction factors of laminated cylindrical panel.

Equation no.RangeParametersEquations

(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)

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