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contributor authorJ. Shewchuk
contributor authorF. A. Roberts
date accessioned2017-05-09T01:38:13Z
date available2017-05-09T01:38:13Z
date copyrightJuly, 1974
date issued1974
identifier issn0094-4289
identifier otherJEMTA8-26837#222_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164812
description abstractA new approach to improving the fatigue resistance of loaded holes in sheet material is presented. The material is first dimpled centering about the region where the hole is to be made, thus introducing tensile plastic strain. The dimple is then flattened and the hole drilled so that the region around the hole is under residual compressive stress. Zero to tension fatigue tests indicate considerable improvement in the fatigue strength of loaded holes as a result of dimpling. A fatigue strength improvement factor of nearly three for 106 cycles to failure was obtained based on the median lives of nominally 0.050-in. thick 2024-T3 aluminum alloy specimens.
publisherThe American Society of Mechanical Engineers (ASME)
titleIncreasing the Fatigue Strength of Loaded Holes by Dimpling
typeJournal Paper
journal volume96
journal issue3
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3443214
journal fristpage222
journal lastpage226
identifier eissn1528-8889
keywordsFatigue strength
keywordsFatigue testing
keywordsSheet materials
keywordsTension
keywordsFatigue
keywordsAluminum alloys
keywordsElectrical resistance
keywordsCompressive stress
keywordsCycles AND Failure
treeJournal of Engineering Materials and Technology:;1974:;volume( 096 ):;issue: 003
contenttypeFulltext


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