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Application of a Cohesive Zone Model for Simulating Fatigue Crack Growth From Moderate to High ΔK Levels of Inconel 718

International Journal of Aerospace Engineering - Egypt
doi 10.1155/2018/4048386
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Abstract

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Categories
Aerospace Engineering
Date

January 1, 2018

Authors
Huan LiJinshan LiHuang Yuan
Publisher

Hindawi Limited


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