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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. (Autor:in) / Mikulova, D. (Autor:in) / Milazzo, A. / Aliabadi, M.H.
01.01.2014
4 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
620.11
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