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Buckling of thin-walled cylinder under axial compression and internal pressure /

An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predi...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Lo, Hsu
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Otros Autores: Crate, Harold, Schwartz, Edward B.
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2021.
Temas:
Acceso en línea:Texto completo
Descripción
Sumario:An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results.
Notas:"January 1950."
NACA TN No. 2021.
Descripción Física:1 online resource (29 pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156195
1680156195
Acceso:Access restricted to Ryerson students, faculty and staff.