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Critical combinations of torsion and direct axial stress for thin-walled cylinders /

A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical c...

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Détails bibliographiques
Cote:Libro Electrónico
Auteur principal: Batdorf, S. B. (Auteur)
Collectivité auteur: Langley Aeronautical Laboratory
Autres auteurs: Stein, Manuel, Schildcrout, Murry
Format: Publication officielle Électronique eBook
Langue:Inglés
Publié: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Collection:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1345.
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