Critical stress of thin-walled cylinders in torsion

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Bibliographic Details
Main Authors Batdorf, S. B. (Author), Stein, Manuel (Author), Schildcrout, Murry (Author)
Corporate Author Langley Aeronautical Laboratory
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 1344.
Subjects
Online AccessFull text
ISBN9781680156041
1680156047
Physical Description1 online resource (21, [5] pages) : illustrations, tables

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Abstract: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
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (21, [5] pages) : illustrations, tables