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contributor authorM. Ramulu
contributor authorM. Hashish
contributor authorJ. Hopkins
contributor authorS. Kunaporn
contributor authorM. Jenkins
date accessioned2017-05-09T00:08:33Z
date available2017-05-09T00:08:33Z
date copyrightFebruary, 2002
date issued2002
identifier issn0094-9930
identifier otherJPVTAS-28414#118_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127386
description abstractAn experimental study of high-pressure waterjet peening on 7075-T6 aluminum alloy was conducted to investigate the effects of waterjet on high-cycle fatigue life and fatigue crack growth. Unnotched hourglass-shaped circular cross section test specimens were fatigue tested in completely reversed rotating bending (R=Smin/Smax=−1) to determine fatigue life behavior (S-N curves). Single-edge-notched flat tensile test specimens were tested in the tension-tension fatigue crack growth tests (R=Smin/Smax=0.1) to determine fatigue crack propagation behavior (da/dN versus ΔK). Surface characteristics and fracture surfaces were evaluated by scanning electron microscopy (SEM). Results show that waterjet peening can increase high-cycle fatigue life, delay fatigue crack initiation, and decrease the rate of fatigue crack propagation.
publisherThe American Society of Mechanical Engineers (ASME)
titleFatigue Performance of High-Pressure Waterjet-Peened Aluminum Alloy
typeJournal Paper
journal volume124
journal issue1
journal titleJournal of Pressure Vessel Technology
identifier doi10.1115/1.1398553
journal fristpage118
journal lastpage123
identifier eissn1528-8978
keywordsFatigue
keywordsAluminum alloys
keywordsShot peening
keywordsHigh pressure (Physics)
keywordsCycles
keywordsFatigue cracks
keywordsFatigue life
keywordsFracture (Process)
keywordsStress
keywordsTension
keywordsDeformation AND Delays
treeJournal of Pressure Vessel Technology:;2002:;volume( 124 ):;issue: 001
contenttypeFulltext


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