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NACA-TR-733

Critical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation along the Unloaded Edges

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:02:57Z
date available2017-09-04T17:02:57Z
date copyright01/01/1942
date issued1942
identifier otherBXWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/126502
description abstractA chart is presented for the values of the coefficient in the formula for the critical compressive stress at which buckling may be expected to occur in flat rectangular plates supported along all edges and, in addition, elastically restrained against rotation along the unloaded edges. The mathematical derivations of the formulas required in the construction of the chart are given.
languageEnglish
titleNACA-TR-733num
titleCritical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation along the Unloaded Edgesen
typestandard
page11
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsALLOYS
subject keywordsALUMINUM
subject keywordsANALYSIS
subject keywordsBUCKLING
subject keywordsCOEFFICIENTS
subject keywordsCOMPRESSION
subject keywordsCONSTRAINTS
subject keywordsCRITICAL
subject keywordsDIFFERENTIAL
subject keywordsEDGE
subject keywordsEDGES
subject keywordsELASTIC
subject keywordsEQUATIONS
subject keywordsFLANGES
subject keywordsFLAT
subject keywordsFORMULAS
subject keywordsLOADING
subject keywordsLOADS
subject keywordsMATHEMATICS
subject keywordsPLATES
subject keywordsPROPERTIES
subject keywordsRECTANGULAR
subject keywordsSUPPORTS


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