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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.

Détails bibliographiques
Cote:Libro Electrónico
Auteur principal: Stein, Manuel
Collectivité auteur: United States. National Advisory Committee for Aeronautics
Autres auteurs: Mayers, J.
Format: Électronique eBook
Langue:Inglés
Publié: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Collection:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2601.
Sujets:
Accès en ligne:Texto completo

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