An edition of Critical combinations of torsion and direct axial stress for thin-walled cylinders
(1947)
Critical combinations of torsion and direct axial stress for thin-walled cylinders
by S. B. Batdorf
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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.
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Subjects
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 stressShowing 1 featured edition. View all 1 editions?
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Critical combinations of torsion and direct axial stress for thin-walled cylinders
1947, National Advisory Committee for Aeronautics
in English
1680156055 9781680156058
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Edition Notes
"Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1345.
Includes bibliographical references (page 25)
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| December 19, 2022 | Created by MARC Bot | import new book |