[1]
H.P. Kan, Final report DOT/FAA/AR-97/79 (1998).
Google Scholar
[2]
E. Demuts, R. S. Sandhu, J.A. Daniels, report N° DOT/FAA/CT-92-25 (1992) 1097 - 1104.
Google Scholar
[3]
S.A. Hitchen and R.M. Kemp, Comp. 26 (1994) 207-214.
Google Scholar
[4]
GS. Hinrich, V. Chen, D. Jegley, L.C. Dickinson and K. Edward, NASA conference publication 3294 (1995).
Google Scholar
[5]
E. Fuoss, P.V. Straznicky, C. Poon, Comp. Struc. 41 ( 1998 ) 67 -77.
Google Scholar
[6]
D.R. Ambur and J.H. Starnes Jr, In structures, structural dynamics, and material conference (1998).
Google Scholar
[7]
N.H. Tai, C.C.M. Ma, J.M. Lin and G.Y. Wu, Comp. Sci. and Tech. 59 (1999) 1753-1762.
Google Scholar
[4]
GS. Hinrich, V. Chen, D. Jegley, L.C. Dickinson and K. Edward, NASA conference publication 3294 (1995).
Google Scholar
[8]
D.D.R. Cartié, P.E. Irving, Comp. part A 33 (2002) 483 - 493.
Google Scholar
[9]
T. Mitrevski, I.H. Marshal, R. Thomson, R. Jones and B. Whittingham, comp. struct. (2004).
Google Scholar
[10]
G. Caprino, P. Iaccarino and A. Lamboglia, Composite structures 88 (2009) 360-366.
Google Scholar
[11]
A. Duarte, I. Herszberg and R. Patton, Composite structures 47 (1999) 753-758.
Google Scholar
[12]
J. Masters, Key Eng. Mater. 37 (1989) 317-348.
Google Scholar
[13]
H. Kishi, M. Kuwata, S. Matsuda, T. Asami and A. Murakami, Composites Science and technology 64 (2004) 2517-2523.
DOI: 10.1016/j.compscitech.2004.05.006
Google Scholar
[14]
Reifsnider, KL, Lesko J, Case S. IUTAM - Symposium on Mechanics of Composite Material (1983); 399-420.
Google Scholar
[15]
Talreja R, Yalvac S, Yats LD, Wetters DG. Transverse cracking and stiffness reduction in cross-ply laminates of different matrix toughness. J of comp mat 1992; - 26(11): 1644-1663.
DOI: 10.1177/002199839202601105
Google Scholar
[16]
Gathercole N, Reiter H, Adam T, Harris B. Life prediction for fatigue of T800/5245 carbonfibre composite : I. Constant-amplitude loading. Int J of Fatigue 1994; 16(8): 523-532.
DOI: 10.1016/0142-1123(94)90478-2
Google Scholar
[17]
Mao H, Mahadevan S. Fatigue damage modelling of composite materials. Comp Struct 2002; 58: 405-410.
DOI: 10.1016/s0263-8223(02)00126-5
Google Scholar
[18]
Dzenis YA. Cycle-based analysis of damage and failure in advanced composites under fatigue: 1. Experimental observation of damage development within loading cycles. Int J of Fatigue 2003; 25(6): 499-510.
DOI: 10.1016/s0142-1123(02)00170-6
Google Scholar
[19]
Gros XE, Bousigue J, Takahashi K. NDT data fusion at pixel level. NDT & E Int 1999; 32(5): 283-292.
DOI: 10.1016/s0963-8695(98)00056-5
Google Scholar
[20]
Vary A. Acousto-Ultrasonics, In: Nondestructive testing of fiber reinforced plastics. Composites 1990; 2: 1-54.
Google Scholar
[21]
Lachaud F., thèse de doctorat, Université Paul Sabatier Toulouse (1997).
Google Scholar
[22]
Smith T.R. and Owen M. J, proceedings of the sixth International reinforced plastics Congress (1968).
Google Scholar
[23]
B. Harris, Fatigue in Composites (2003).
Google Scholar
[24]
C. Bathias, Eng. Fract. Mech. 40 (1991) 757 -783.
Google Scholar
[25]
M.H. Behesty and B. Harris, In : ICFC 1 (1997) 365-372.
Google Scholar
[26]
L. Minnetyan, Computational simulation of composite structural fatigue, report NASA/CR_2005-213573 ( 2005).
Google Scholar
[27]
T.P. Philippidis and V.A. Passipoularidis, Int. J. Fat. 29 (2007) 2104-2116.
Google Scholar
[28]
N.L. Post, S.W. Case, J.J. Lesko, Int. J. Fatigue ( 2008 ) 2064 - (2086).
Google Scholar