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NACA-ARR-L5B10

Effect of normal pressure on the critical compressive and shear stress of curved sheet

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:45:16Z
date available2017-09-04T18:45:16Z
date copyright03/01/1945
date issued1945
identifier otherKGYHUEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1216AF679D40527318548F1EFDEC014A/handle/yse/226733
description abstractResults are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheets. It was found that normal pressure raised the critical compressive and shear stress of curved sheets except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure. (author)
languageEnglish
titleNACA-ARR-L5B10num
titleEffect of normal pressure on the critical compressive and shear stress of curved sheeten
typestandard
page16
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1945
contenttypefulltext
subject keywordsALUMINUM ALLOYS
subject keywordsATMOSPHERIC PRESSURE
subject keywordsAXIAL COMPRESSION LOADS
subject keywordsBOXES
subject keywordsBUCKLING
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsCRITICAL LOADING
subject keywordsCURVED PANELS
subject keywordsLOAD TESTS
subject keywordsPRESSURE EFFECTS
subject keywordsRIBS (SUPPORTS)
subject keywordsSHEAR STRENGTH
subject keywordsSHEAR STRESS
subject keywordsSHEETS
subject keywordsTORSIONAL STRESS


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