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NACA-TR-636

Approximate Stress Analysis of Multistringer Beams with Shear Deformation of the Flanges

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:04:07Z
date available2017-09-04T18:04:07Z
date copyright01/01/1938
date issued1938
identifier otherGFYHUEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/187012
description abstractThe problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere.
languageEnglish
titleNACA-TR-636num
titleApproximate Stress Analysis of Multistringer Beams with Shear Deformation of the Flangesen
typestandard
page21
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1938
contenttypefulltext
subject keywordsAIRCRAFT STRUCTURES
subject keywordsAXIAL COMPRESSION LOADS
subject keywordsBEAMS (SUPPORTS)
subject keywordsDEFORMATION
subject keywordsFLANGES
subject keywordsFORMULAS
subject keywordsNUMERICAL ANALYSIS
subject keywordsRIBS (SUPPORTS)
subject keywordsSHEAR STRESS
subject keywordsSTRESS ANALYSIS
subject keywordsSTRESSED-SKIN STRUCTURES
subject keywordsSTRINGERS
subject keywordsWINGS


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