Critical stress of thin-walled cylinders in torsion

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 r...

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Bibliographic Details
Main Authors: Batdorf, S. B., (Author), Stein, Manuel, (Author), Schildcrout, Murry, (Author)
Corporate Author: Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1344.
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ISBN: 9781680156041
1680156047
Physical Description: 1 online resource (21, [5] pages) : illustrations, tables

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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.
Item Description: "Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1344.
Bibliography: Includes bibliographical references (page 19)
ISBN: 9781680156041
1680156047
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