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NASA-TN-D-3879

Investigation of fatigue crack growth in Ti-8Al-1Mo-1V (duplex-annealed) specimens having various widths

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1967

Abstract: Axial-load fatigue crack propagation tests on duplex annealed titanium alloy specimens having various widths.
URI: http://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/207330
Subject: ANNEALING
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-TN-D-3879

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:25:04Z
date available2017-09-04T18:25:04Z
date copyright01/01/1967
date issued1967
identifier otherIIBBFEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/207330
description abstractAxial-load fatigue crack propagation tests on duplex annealed titanium alloy specimens having various widths.
languageEnglish
titleNASA-TN-D-3879num
titleInvestigation of fatigue crack growth in Ti-8Al-1Mo-1V (duplex-annealed) specimens having various widthsen
typestandard
page22
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1967
contenttypefulltext
subject keywordsANNEALING
subject keywordsAXIAL LOADS
subject keywordsCRACK PROPAGATION
subject keywordsDUPLEXERS
subject keywordsFATIGUE (MATERIALS)
subject keywordsFATIGUE TEST
subject keywordsFATIGUE TESTS
subject keywordsTITANIUM ALLOY
subject keywordsTITANIUM ALLOYS
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DSpace software copyright © 2017-2020  DuraSpace
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