Article Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056
Waman Vishwanath Vaidya, Manfred Horstmann, Kandasamy Angamuthu, Mustafa Koçak
2010
Vaidya, Waman Vishwanath, Horstmann, Manfred, Angamuthu, Kandasamy and Koçak, Mustafa. "Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056" Materials Testing, vol. 52, no. 11-12, 2010, pp. 771-777. https://doi.org/10.3139/120.110185
Vaidya, W., Horstmann, M., Angamuthu, K. & Koçak, M. (2010). Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056. Materials Testing, 52(11-12), 771-777. https://doi.org/10.3139/120.110185
Vaidya, W., Horstmann, M., Angamuthu, K. and Koçak, M. (2010) Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056. Materials Testing, Vol. 52 (Issue 11-12), pp. 771-777. https://doi.org/10.3139/120.110185
Vaidya, Waman Vishwanath, Horstmann, Manfred, Angamuthu, Kandasamy and Koçak, Mustafa. "Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056" Materials Testing 52, no. 11-12 (2010): 771-777. https://doi.org/10.3139/120.110185
Vaidya W, Horstmann M, Angamuthu K, Koçak M. Utilising CODmax as an Indirect Fatigue Crack Length Measurement Parameter for M(T) Specimens of an Airframe Aluminium Alloy AA6056. Materials Testing. 2010;52(11-12): 771-777. https://doi.org/10.3139/120.110185
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