• 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-WRL-258

EFFECT OF NORMAL PRESSURE ON THE CRITICAL COMPRESSIVE STRESS OF CURVED SHEET

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1942

Abstract: Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. (author)
URI: https://yse.yabesh.ir/std/handle/yse/111429
Subject: ATMOSPHERIC PRESSURE
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (465.9Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NACA-WRL-258

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:48:00Z
date available2017-09-04T16:48:00Z
date copyright08/25/1942
date issued1942
identifier otherWGYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/111429
description abstractResults are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. (author)
languageEnglish
titleNACA-WRL-258num
titleEFFECT OF NORMAL PRESSURE ON THE CRITICAL COMPRESSIVE STRESS OF CURVED SHEETen
typestandard
page9
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsATMOSPHERIC PRESSURE
subject keywordsBUCKLING
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsCRITICAL LOADING
subject keywordsCURVED PANELS
subject keywordsLOAD TESTS
subject keywordsPRESSURE EFFECTS
subject keywordsREINFORCEMENT (STRUCTURES)
subject keywordsRIBS (SUPPORTS)
subject keywordsSHEETS
subject keywordsSPACING
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