A simply supported, specially orthotropic plate is subjected to an in-plane compressive load per unit length (N_{x})
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A simply supported, specially orthotropic plate is subjected to an in-plane compressive load per unit length \(N_{x}\) and an in-plane tensile load per unit length \(N_{y}=-0.5 N_{x}\) as shown in Figure 7.69. Derive the expression for the critical buckling load.
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Related Book For 
Principles Of Composite Material Mechanics
ISBN: 9781498720694
4th Edition
Authors: Ronald F. Gibson
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