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NACA-TN-929

Analysis of circular shell-supported frames

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:00:21Z
date available2017-09-04T18:00:21Z
date copyright01/01/1944
date issued1944
identifier otherFWITDEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/183338
description abstractIn the past it has been customary to analyze shell-supported frames on the basis of the assumption that frame bending distortion does not affect the character of the sheer resistance in the skin. This assumption has been found to be considerably in error for a majority of practical cases.
In order to obtain results more nearly representing the actual case, it is essential that the deformation of  the frame and the deformation of the shell be consistent with each other. While this principle of "consistent deformations" is already wall known and appreciated, its application to fuselage frame analysis and similar problems has not been extensively developed.
languageEnglish
titleNACA-TN-929num
titleAnalysis of circular shell-supported framesen
typestandard
page84
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1944
contenttypefulltext
subject keywordsBENDING
subject keywordsDEFORMATION
subject keywordsDISTORTION
subject keywordsFORMS
subject keywordsFRAMES
subject keywordsFUSELAGES
subject keywordsMEMBER
subject keywordsSHEAR
subject keywordsSHELLS
subject keywordsSKIN
subject keywordsSTRENGTH
subject keywordsSTRUCTURAL
subject keywordsSUPPORTS


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