Title Critical combinations of torsion and direct axial stress for thin-walled cylinders / by S.B. Batdort, Manuel Stein and Murry Schildcrout

Published Washington, D.C. : National Advisory Committee for Aeronautics, 1947

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Description 1 online resource (28, [8] pages) : illustrations, tables Series National Advisory Committee for Aeronautics technical note ; no. 1345 Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1345. Summary 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 Notes "Langley Memorial Aeronautical Laboratory." Date of issue: June 1947 Report no. NACA TN No. 1345 Bibliography Includes bibliographical references (page 25) Notes Print version record Subject Shells (Engineering) Thin-walled structures. Cylinders. Strains and stresses. Torsion. Buckling (Mechanics) shell structures. cylinders (solids) torsional stress. Thin-walled structures Shells (Engineering) Buckling (Mechanics) Cylinders Strains and stresses Torsion Form Electronic book Author Stein, Manuel Schildcrout, Murry United States. National Advisory Committee for Aeronautics, issuing body. Langley Aeronautical Laboratory. ISBN 9781680156058 1680156055

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