Classical laminate plate theory model
2016-08-23
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Based on the classic calculation of composite laminates plates when the tensile and flexural stress-strain distribution, can be arbitrarily set the plates in the thickness of each layer, the orientation angle. Extractable plate film strains and curvature, then get the stress and strain of each layer (including spindle orientation and direction of offset-axes)
matlab
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经典
理论
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