Probability modelling and statistical analysis of damage in the lower wing skins of two retired B‐707 aircraft
暂无分享,去创建一个
[1] Robert P. Wei,et al. A probability model for the growth of corrosion pits in aluminum alloys induced by constituent particles , 1998 .
[2] D. G. Harlow,et al. Probabilities of occurrence and detection of damage in airframe materials , 1999 .
[3] R. Wei,et al. Probability approach for prediction of corrosion and corrosion fatigue life , 1994 .
[4] R. Wei,et al. Transition from pitting to fatigue crack growth—modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy , 1996 .
[5] Lee,et al. The effect of pitting corrosion on fatigue life , 2000 .
[6] Robert P. Wei,et al. Environmental fatigue crack propagation of aluminum alloys at low stress intensity levels , 1970 .
[7] Chi-Min Liao. Particle-induced pitting corrosion of aluminum alloys , 1998 .
[8] Robert P. Wei,et al. A technique for studying the 3-dimensional shape of corrosion pits , 1996 .