[1]
P. Mathivanan, M. Balakrishnan and H. Krishnan. Hybrid Laminates Metal Thickness, Fiber Volume Fraction Effect on the Tensile Properties, Debonding of Hybrid Laminates[J]. Journal of Reinforced Plastics and Composites, 2010(14), Vol. 29: 112-120.
DOI: 10.1177/0731684409345616
Google Scholar
[2]
G. Allegri, M.R. Wisnom, S.R. Hallett. A simplified approach to the damage tolerance design of asymmetric tapered laminates. Part I: Methodology development[J]. Composites Part A: Applied Science and Manufacturing, 2010, 41(10): 1388~1394.
DOI: 10.1016/j.compositesa.2010.05.009
Google Scholar
[3]
A. Vlot. Glare, History of the Development of a New Aircraft Material[M]. Kluwer Academic Publishers, 2001, 35~36.
Google Scholar
[4]
Lucas P Durand, Composite Materials Research Progress[M]. Nova Science Publishers, Inc. 2008, 13~14.
Google Scholar
[5]
B. Kolesnikov, L. Herbeck, A. Fink. CFRP/titanium hybrid material for improving composite bolted joints[J]. Composite Structures, 2008, 83(4): 368~370.
DOI: 10.1016/j.compstruct.2007.05.010
Google Scholar
[6]
D. A. Burianek, A. E. Giannakopoulos, S. M. Spearing. Modeling of facesheet crack growth in titanium–graphite hybrid laminates, Part I[J]. Engineering Fracture Mechanics, 2003, 70(6): 775~778.
DOI: 10.1016/s0013-7944(02)00086-3
Google Scholar
[7]
P. Corte´s , W.J. Cantwell. The prediction of tensile failure in titanium-based thermoplastic fibre–metal laminates[J], Composites Science and Technology 66 (2006): 2306–2316.
DOI: 10.1016/j.compscitech.2005.11.031
Google Scholar
[8]
M. A. Shayed, Ch. Cherif, R. D. Hund , T. Cheng, F. Osterod Carbon and Glass Fibers Modified by Polysilazane Based Thermal Resistant Coating[J] Textile Research Journal Vol 80(11): 1118–1128.
DOI: 10.1177/0040517509357648
Google Scholar
[9]
R. R. Habeb, G. S. Walker, I. A. Jones. etc. Fabrication Effects on Properties of Composites for Medical Applications: 1. CompositePreparation and Characterization[J]. Journal of Reinforced Plastics and Composites, 2011, 29(1): 112-123.
DOI: 10.1177/0731684408096425
Google Scholar
[10]
Shang-Lin Gao, Jang-Kyo Kim. Cooling rate in-uences in carbon fibre/PEEK composites. Part II: interlaminar fracture toughness[J], Composites: Part A 32 (2001) 763-774.
DOI: 10.1016/s1359-835x(00)00188-3
Google Scholar
[11]
Z. Mikulik, D. W. Kelly, R. S. Thomson etc . Fracture mechanics based predictions of initiation and growth of multi-level delaminations in a composite specimen[J]. International Journal of Fracture, 2010, 170( 2): 145-157.
DOI: 10.1007/s10704-011-9619-5
Google Scholar
[12]
C.A. Rideout, S. C Taylor. Advanced deep focus acoustic microscope for nondestructive inspection of metals and composite materials[J]. Aerospace conference, 2009 IEEE: 1 – 10.
DOI: 10.1109/aero.2009.4839664
Google Scholar
[13]
S. Ksouri1, M. Matmat, H. Boukabache, etc. Damage detection in composite laminates aeronautics structures through accelerometers network[J]. Journal Advances in Materials Sciences, 2011, 11(2): 37-43.
DOI: 10.2478/v10077-011-0009-5
Google Scholar
[14]
Wei Jia-shun, Pan Lei, Tao Jie, et al. The influence of surface treatment on the wettability of carbon fiber and the tensile strength of CFRP. Fiber Composites, 2010(4): 36-40.
Google Scholar