Title Critical stress of thin-walled cylinders in torsion / 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 (21, [5] pages) : illustrations, tables Series National Advisory Committee for Aeronautics technical note ; no. 1344 Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1344. Summary A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions Notes "Langley Memorial Aeronautical Laboratory." Date of issue: June 1947 Report no. NACA TN No. 1344 Bibliography Includes bibliographical references (page 19) Notes Print version record Subject Shells (Engineering) -- Thin-walled structures Cylinders. Strains and stresses. Torsion. cylinders (solids) torsional stress. Cylinders Strains and stresses Torsion Form Electronic book Author Stein, Manuel, author Schildcrout, Murry, author United States. National Advisory Committee for Aeronautics, issuing body. Langley Aeronautical Laboratory. ISBN 9781680156041 1680156047

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