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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. (author) / Horstmann, M. (author) / Angamuthu, K. (author) / Kocak, M. (author)
MATERIALPRUFUNG ; 52 ; 771-777
2010-01-01
7 pages
Article (Journal)
English
DDC:
620
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