Fatigue crack growth in fiber-metal laminates

[1]  Lei Zhang,et al.  Numerical analysis of delamination buckling and growth in slender laminated composite using cohesive element method , 2010 .

[2]  D. Borst,et al.  Analysis of fracture and delamination in laminates using 3D numerical modelling , 2009 .

[3]  Jenn‐Ming Yang,et al.  Modeling of fatigue crack growth in notched fiber metal laminates , 2008 .

[4]  Ireneusz Lapczyk,et al.  Progressive damage modeling in fiber-reinforced materials , 2007 .

[5]  René Alderliesten,et al.  Fatigue and damage tolerance issues of GLARE in aircraft structures , 2006 .

[6]  Takashi Matsumura,et al.  Evaluation of fatigue crack growth behavior of GLARE3 fiber/metal laminates using a compliance method , 2003 .

[7]  René Alderliesten,et al.  Fatigue crack growth prediction in GLARE hybrid laminates , 2003 .

[8]  X.R. Wu,et al.  A THEORETICAL MODEL FOR PREDICTING FATIGUE CRACK GROWTH RATES IN FIBRE‐REINFORCED METAL LAMINATES , 1998 .

[9]  R. Marissen,et al.  Fatigue crack growth in ARALL. A hybrid aluminium-aramid composite material: Crack growth mechanisms and quantitative predictions of the crack growth rates , 1988 .

[10]  Zhu Bin.  COMPARISON OF GLARE LAMINATE WITH ALUMINUM ALLOY AND ITS APPLICATION , 2006 .

[11]  Liang Zhong-quan,et al.  PERFORMANCE AND APPLICATION OF GLARE LAMINATES IN A380 AIRLINER , 2005 .

[12]  J. Yang,et al.  The mechanical behavior of GLARE laminates for aircraft structures , 2005 .

[13]  A. Vlot,et al.  Glare: History of the Development of a New Aircraft Material , 2001 .

[14]  Brian N. Cox,et al.  Life Prediction for Bridged Fatigue Cracks , 1996 .