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.
Temas:
Shells (Engineering)
Thin-walled structures.
Cylinders.
Strains and stresses.
Torsion.
Buckling (Mechanics)
Coques (Ingénierie)
Structures à parois minces.
Cylindres.
Contraintes (Mécanique)
Torsion (Mécanique)
Flambage (Résistance des matériaux)
shell structures.
cylinders (solids)
torsional stress.
Acceso en línea:Texto completo
Descripción
Sumario: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 curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations.
Notas:"Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1345.
Descripción Física:1 online resource (28, [8] pages) : illustrations, tables
Bibliografía:Includes bibliographical references (page 25)
ISBN:9781680156058
1680156055

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