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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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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Batdorf, S. B. (Autor)
Autor Corporativo: Langley Aeronautical Laboratory
Otros Autores: Stein, Manuel, Schildcrout, Murry
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1345.
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