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Utilising COD~m~a~x as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056
Utilising COD~m~a~x as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056
Utilising COD~m~a~x as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056
Vaidya, W.V. (Autor:in) / Horstmann, M. (Autor:in) / Angamuthu, K. (Autor:in) / Kocak, M. (Autor:in)
MATERIALPRUFUNG ; 52 ; 771-777
01.01.2010
7 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
620
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