Multiaxial fatigue life prediction of composite materials
composite materials、fatigue life、damage parameter、material properties、boundary conditions、prediction method、unit cell model、matrix cracking、test condition、filament wound、mode of
30
V21;TG1
The authors appreciate the supports from the Jiangsu Province Key Laboratory of Aerospace Power System of ChinaNJ20140019;the National Natural Science Foundation of China51205190
2017-07-13(万方平台首次上网日期,不代表论文的发表时间)
共9页
1012-1020