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NACA-WRL-67

The Effect of Internal Pressure on the Buckling Stress of Thin Walled Circular Cylinders Under Torsion

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:24:00Z
date available2017-09-04T15:24:00Z
date copyright01/01/1940
date issued1940
identifier otherNGYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/24353
description abstractThe results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived. (author)
languageEnglish
titleNACA-WRL-67num
titleThe Effect of Internal Pressure on the Buckling Stress of Thin Walled Circular Cylinders Under Torsionen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1940
contenttypefulltext
subject keywordsBUCKLING
subject keywordsCIRCULAR CYLINDERS
subject keywordsCRITICAL LOADING
subject keywordsCURVED PANELS
subject keywordsINTERNAL PRESSURE
subject keywordsPRESSURE EFFECTS
subject keywordsREINFORCED SHELLS
subject keywordsREINFORCEMENT RINGS
subject keywordsSHEAR STRESS
subject keywordsSKIN (STRUCTURAL MEMBER)
subject keywordsSTIFFENING
subject keywordsSTRUCTURAL FAILURE
subject keywordsTESTS
subject keywordsTHEORIES
subject keywordsTHIN WALLED SHELLS
subject keywordsTORSIONAL STRESS


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