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Evaluation of Overloading and Crack Closure Effects on Fatigue Crack Growth in an Aircraft 7075-T7351 Al-Alloy
Evaluation of Overloading and Crack Closure Effects on Fatigue Crack Growth in an Aircraft 7075-T7351 Al-Alloy
Evaluation of Overloading and Crack Closure Effects on Fatigue Crack Growth in an Aircraft 7075-T7351 Al-Alloy
Cerny, I. (author) / Mikulova, D. (author) / Milazzo, A. / Aliabadi, M.H.
2014-01-01
4 pages
Article (Journal)
English
DDC:
620.11
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