New Model and Analytical Review of Approaches to Buckling Problem Investigation of Structurally Anisotropic Aircraft Panels Made from Composite Materials

Gavva, L. M.

doi:10.1007/978-981-15-1773-0_12

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New Model and Analytical Review of Approaches to Buckling Problem Investigation of Structurally Anisotropic Aircraft Panels Made from Composite Materials

Cited by 3 publications

References 34 publications

An Experimental Study on Residual Stresses and the Evaluation of Performance of Polymer Composite Materials

An Experimental Study on Residual Stresses and the Evaluation of Performance of Polymer Composite Materials

Manipulation of optimal size-weight project parameters of composite structurally anisotropic aircraft panels with restrictions according to the refined buckling theory

Analysis and selection of optimum composite floor panel

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