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contributor authorR. P. Hubbard
date accessioned2017-05-09T00:20:03Z
date available2017-05-09T00:20:03Z
date copyrightDecember, 1969
date issued1969
identifier issn0098-2202
identifier otherJFEGA4-27348#625_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133790
description abstractAn investigation was made of fatigue crack growth in notched samples of 7075-T6 aluminum alloy which were subjected to cyclic compressive loading. Photoelastic techniques were employed to determine plastic strain distribution in the vicinity of the notch at different load levels. A fracture mechanics model relating crack growth to residual tensile stress at the notch root is proposed. Validity of the model is examined by comparing calculated stress intensity values based on the model with stress intensity values determined from the observed growth rate data.
publisherThe American Society of Mechanical Engineers (ASME)
titleCrack Growth Under Cyclic Compression
typeJournal Paper
journal volume91
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3571200
journal fristpage625
journal lastpage630
identifier eissn1528-901X
keywordsFracture (Materials)
keywordsCompression
keywordsStress
keywordsFracture mechanics
keywordsAluminum alloys
keywordsFatigue cracks AND Tension
treeJournal of Fluids Engineering:;1969:;volume( 091 ):;issue: 004
contenttypeFulltext


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