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A simplified method of elastic-stability analysis for thin cylindrical shells /

This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is appli...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Batdorf, S. B.
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : U.S. G.P.O., 1947.
Colección:Report (United States. National Advisory Committee for Aeronautics) ; no. 874.
Temas:
Acceso en línea:Texto completo
Descripción
Sumario:This paper develops a new method for determining the buckling stresses of cylindrical shells under various loading conditions. In part I, the equation for the equilibrium of cylindrical shells introduced by Donnell in NACA report no. 479 to find the critical stresses of cylinders in torsion is applied to find critical stresses for cylinders with simply supported edges under other loading conditions. In part II, a modified form of Donnell's equation for the equilibrium of thin cylindrical shells is derived which is equivalent to Donnell's equation but has certain advantages in physical interpretation and in ease of solution, particularly in the case of shells having clamped edges. --
Descripción Física:1 online resource (25 pages)
Bibliografía:Includes bibliographical references.
ISBN:9781680156454
1680156454