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NACA-TR-827

Charts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:34:58Z
date available2017-09-04T16:34:58Z
date copyright01/01/1945
date issued1945
identifier otherUYWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/98511
description abstractDesign charts are developed for 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners. These charts make possible the design of the lightest panels of this type for a wide range of design requirements. Examples of the use of the charts are given and it is pointed out on the basis of these examples that, over a wide range of design conditions, the maintenance of buckle-free surfaces does not conflict with the achievement of high structural efficiency. The achievement of the maximum possible structural efficiency with 24s-t aluminum-alloy panels, however, requires closer stiffener spacings than those now in common use.
languageEnglish
titleNACA-TR-827num
titleCharts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffenersen
typestandard
page28
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1945
contenttypefulltext
subject keywordsALLOYS
subject keywordsALUMINUM
subject keywordsBUCKLING
subject keywordsCHARTS
subject keywordsCOMPRESSION
subject keywordsCOMPRESSIVE
subject keywordsDESIGN
subject keywordsFLAT
subject keywordsLOADS
subject keywordsPANELS
subject keywordsPLATES
subject keywordsREINFORCED
subject keywordsSKIN
subject keywordsSTIFFENING
subject keywordsSTRENGTH
subject keywordsSTRESSED
subject keywordsSTRUCTURES


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