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Compressive buckling of simply supported curved plates and cylinders of sandwich construction /

Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Stein, Manuel
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Otros Autores: Mayers, J.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2601.
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Acceso en línea:Texto completo

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