Show simple item record

NACA-TR-734

Critical Compressive Stress for Outstanding Flanges

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:50:51Z
date available2017-09-04T17:50:51Z
date copyright01/01/1942
date issued1942
identifier otherEXWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/174118
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 outstanding flanges. These flanges are flat rectangular plates supported along the loaded edges, supported and elastically restrained along one unloaded edge, and free along the other unloaded edge. The mathematical derivations of the formulas required for construction of the chart are given.
languageEnglish
titleNACA-TR-734num
titleCritical Compressive Stress for Outstanding Flangesen
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


Files in this item

Thumbnail
Name:
EXWUYDAAAAAAAAAA.pdf
Size:
557.7Kb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record