Variations in maximum stresses with changes in Poisson's ratio are presented for thin parallelogrammic panels with nonlinear behavior; outline of method solution for governing Von Karman equations is given and it is shown that influence of Poisson's ratio on maximum center and edge stresses depends on skew, aspect ratio, and ratio of deflection to thickness of panel.
Influence of Poisson's ratio on maximum stress in thin parallelogrammic panels
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 13 , n 7
1967
3 pages
Article (Journal)
English
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Theoretical and experimental investigations of thin parallelogrammic panels
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