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A simplified method of elastic-stability analysis for thin cylindrical shells I : Donnell's equation

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:19:49Z
date available2017-09-04T15:19:49Z
date copyright01/01/1947
date issued1947
identifier otherMUMSYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/19693
description abstractThe equation for the equilibrium of cylindrical shells introduced by Donnell in NACA Technical Report no. 479 to find the critical stresses of cylinders in torsion is applied to find critical stresses for cylinders with simply supported edges under other loading conditions. It is shown that by this method solutions may be obtained very easily and the results in each case may be expressed in terms of two nondimensional parameters, one dependent on the critical stress and the other essentially determined by the geometry of the cylinder. The influence of boundary conditions related to edge displacements in the shell median surface is discussed. The accuracy of the solutions found is established by comparing them with previous theoretical solutions and with test results. The solutions to a number of problems concerned with the buckling of cylinders with simply supported edges on the basis of a unified viewpoint are presented in a convenient form for practical use. (author)
languageEnglish
titleNACA-TN-1341num
titleA simplified method of elastic-stability analysis for thin cylindrical shells I : Donnell's equationen
typestandard
page54
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsANALYSIS
subject keywordsAXIAL
subject keywordsBOUNDARY
subject keywordsBUCKLING
subject keywordsCOMPRESSION
subject keywordsCRITICAL
subject keywordsCYLINDRICAL
subject keywordsDISPLACEMENT
subject keywordsDONNELL
subject keywordsEDGES
subject keywordsEQUATIONS
subject keywordsEQUILIBRIUM
subject keywordsHYDROSTATIC
subject keywordsINDEPENDENT
subject keywordsLOADING
subject keywordsLOADS
subject keywordsMATHEMATICS
subject keywordsMEMBER
subject keywordsPRESSURE
subject keywordsPROBLEMS
subject keywordsSHEAR
subject keywordsSHELLS
subject keywordsSKIN
subject keywordsSTRESS
subject keywordsSTRUCTURAL
subject keywordsSUPPORTS
subject keywordsTHIN
subject keywordsTORSION
subject keywordsVALUE
subject keywordsVARIABLES
subject keywordsWALLED


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