Aero-engine Blade Fatigue Analysis Based on Nonlinear Continuum Damage Model Using Neural Networks
Neural Networks、Damage Model、Based
25
TU5;TD8
National Natural Science Foundation of ChinaGrant 60879002;Tianjin Municipal Science and Technology Support Plan of ChinaGrant 10ZCKFGX03800
2012-06-26(万方平台首次上网日期,不代表论文的发表时间)
共8页
338-345