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NACA-TN-1344

CRITICAL STRESS OF THIN-WALLED CYLINDERS IN TORSION

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1947

Abstract: A theoretical solution is given for 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.
URI: https://yse.yabesh.ir/std/handle/yse/13135
Subject: CYLINDERS
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NACA-TN-1344

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:14:20Z
date available2017-09-04T15:14:20Z
date copyright06/01/1947
date issued1947
identifier otherMCYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/13135
description abstractA theoretical solution is given for 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.
languageEnglish
titleNACA-TN-1344num
titleCRITICAL STRESS OF THIN-WALLED CYLINDERS IN TORSIONen
typestandard
page34
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsCYLINDERS
subject keywordsCYLINDERS - STRESSES
subject keywordsLOADS - CYLINDERS
subject keywordsSTRESSED SKIN - CYLINDERS
subject keywordsTHEORIES - TORSION & BENDING - DONNELL
subject keywordsTHIN - BUCKLING
subject keywordsTHIN - TORSION
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