Fatigue characteristics of quasi-isotropic CFRP laminates subjected to variable amplitude cyclic two-stage loading
暂无分享,去创建一个
[1] Satoshi Kobayashi,et al. Damage mechanics characterization of transverse cracking behavior in quasi-isotropic CFRP laminates with interlaminar-toughened layers , 2002 .
[2] N. Himmel,et al. A new cumulative fatigue damage model for fibre-reinforced plastics , 2000 .
[3] M. Rigamonti,et al. Tension fatigue analysis and life prediction for composite laminates , 1989 .
[4] S. Mahadevan,et al. Fatigue damage modelling of composite materials , 2002 .
[5] Luo Xu. Interaction between matrix cracking and edge delamination in composite laminates , 1994 .
[6] Zvi Hashin,et al. Cumulative damage theory for composite materials: Residual life and residual strength methods , 1985 .
[7] Douglas L. Jones,et al. Load Sequence Effects on Graphite/Epoxy [±35] 2s Laminates , 1983 .
[8] J. Tong. Characteristics of fatigue crack growth in GFRP laminates , 2002 .
[9] E. K. Gamstedt,et al. An experimental investigation of the sequence effect in block amplitude loading of cross-ply composite laminates , 2002 .
[10] Nobuo Takeda,et al. Effects of toughened interlaminar layers on fatigue damage progress in quasi-isotropic CFRP laminates , 1999 .
[11] J. Rebiere,et al. Initiation and growth of transverse and longitudinal cracks in composite cross-ply laminates , 2001 .
[12] J. Nairn,et al. Fracture Mechanics Analysis of Composite Microcracking: Experimental Results in Fatigue , 1990 .
[13] Asd Wang,et al. Effects of a 90° ply on matrix cracks and edge delamination in composite laminates , 1990 .