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NACA-TN-3431

An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringe

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:06:32Z
date available2017-09-04T15:06:32Z
date copyright03/01/1955
date issued1955
identifier otherLEYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/4024
description abstractA method of strength analysis of short sheet-stringer panels subjected to compression is presented which takes into account the effect that the riveted attachments between the plate and the stiffeners have on the strength of the panels. An analysis of experimental data shows that panel strength is highly influenced by rivet pitch, diameter, and location and that the degree of influence for a given riveting depends on the panel configuration and panel material. (author)
languageEnglish
titleNACA-TN-3431num
titleAn Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringeen
typestandard
page50
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
subject keywordsALUMINUM ALLOYS
subject keywordsBUCKLING
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsCONNECTORS
subject keywordsDIAMETERS
subject keywordsFLAT PLATES
subject keywordsLOAD TESTS
subject keywordsNUMERICAL ANALYSIS
subject keywordsPITCH (INCLINATION)
subject keywordsPOSITION (LOCATION)
subject keywordsPREDICTION ANALYSIS TECHNIQUES
subject keywordsREINFORCEMENT (STRUCTURES)
subject keywordsRIVETED JOINTS
subject keywordsSHEETS
subject keywordsSTIFFENING
subject keywordsSTRESS ANALYSIS
subject keywordsSTRESSED-SKIN STRUCTURES
subject keywordsSTRINGERS
subject keywordsSTRUCTURAL FAILURE
subject keywordsWING PANELS
subject keywordsWRINKLING


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