• 0
    • ارسال درخواست
    • حذف همه
    • Industrial Standards
    • Defence Standards
  • درباره ما
  • درخواست موردی
  • فهرست استانداردها
    • Industrial Standards
    • Defence Standards
  • راهنما
  • Login
  • لیست خرید شما 0
    • ارسال درخواست
    • حذف همه
View Item 
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  • All Fields
  • Title(or Doc Num)
  • Organization
  • Year
  • Subject
Advanced Search
JavaScript is disabled for your browser. Some features of this site may not work without it.

Archive

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

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1955

Abstract: A 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)
URI: https://yse.yabesh.ir/std/handle/yse/4024
Subject: ALUMINUM ALLOYS
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (2.162Mb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-TN-3431

Show full item record

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
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian
 
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian