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NASA-TN-D-3149

Influence of programming techniques and of varying limit load factor on maneuver load fatigue test results

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:18:05Z
date available2017-09-04T15:18:05Z
date copyright01/01/1966
date issued1966
identifier otherMPBBFEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/17644
description abstractVariable amplitude axial load fatigue test on notched aluminum alloy specimens - aircraft component testing.
languageEnglish
titleNASA-TN-D-3149num
titleInfluence of programming techniques and of varying limit load factor on maneuver load fatigue test resultsen
typestandard
page17
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1966
contenttypefulltext
subject keywordsAIRCRAFT PART
subject keywordsAIRCRAFT PARTS
subject keywordsALUMINUM ALLOY
subject keywordsALUMINUM ALLOYS
subject keywordsAXIAL LOAD
subject keywordsAXIAL LOADS
subject keywordsFATIGUE TEST
subject keywordsFATIGUE TESTS
subject keywordsLOAD TESTS
subject keywordsLOADS (FORCES)
subject keywordsMETAL FATIGUE
subject keywordsNOTCH TESTS
subject keywordsNOTCHED METAL


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