MULTI-SITE DAMAGE OF AIRCRAFT COMPONENTS
暂无分享,去创建一个
[1] Hirokazu Shoji,et al. A Bayesian evaluation of simulation models of multiple-site fatigue cracks , 2001 .
[2] Satya N. Atluri,et al. The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures , 1997 .
[3] G. I. Schuëller,et al. A probabilistic criterion for evaluating the goodness of fatigue crack growth models , 1996 .
[4] Roberto Galatolo,et al. An Experimental and Numerical Analysis of Multi-Site Damaged Butt-Joints , 1999 .
[5] Satya N. Atluri,et al. Analytical solution for embedded elliptical cracks, and finite element alternating method for elliptical surface cracks, subjected to arbitrary loadings , 1983 .