American Society for Testing and Materials. ASTM D5528—01: Standard test method for mode Ⅰ interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites [S]. United States: ASTM, 2001.
American Society for Testing and Materials. ASTM D6671/D6671M—06: Standard test method for mixed mode Ⅰ-mode Ⅱ interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites [S]. United States: ASTM, 2006.
[4]
Turon Albert, Davila Carlos G, Camanho Pedro P, et al. An engineering solution for using coarse meshes in the simulation of delamination with cohesive zone models, NASA/TM-2005-213547 .Hampton, VA: NASA Langley Research Center, 2005.
[5]
Turon Albert,Camanho Pedro P, Costa Josep, et al. An interface damage model for the simulation of delamination under variable-mode ratio in composite materials, NASA/TM-2004-213277 . Hampton, VA: NASA Langley Research Center, 2004.
[6]
Yan Aimin, Marechal E, Dang H Nguyen, et al. A finite-element model of mixed-mode delamination in laminated composites with an R-curve effect [J]. Composite Science and Technology, 2001, 61(10): 1413-1427.
[7]
范学领, 孙 秦, 原梅妮, 菊池正纪. 裂纹间距及铺层角度对复合材料分层的影响 [J]. 固体火箭技术, 2009, 32(3): 327-330. Fan Xueling, Sun Qin, Yuan Meini, Kikuchi Masanon. The effect of crack distance and fiber angle on delaminations in laminated composites [J]. Journal of Solid Rocket Technology, 2009, 32(3): 327-330.
[8]
Camanho Pedro P, Davila Carlos G. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials, NASA/TM-2002-211737 . Hampton, VA: NASA Langley Research Center, 2002.
[9]
Naghipour P, Bartsch M, Chernova L, et al. Effect of fiber angle orientation and stacking sequence on mixed mode fracture [J]. Materials Science and Engineering A, 2010, 527(3): 509-517.
[10]
Leslie Banks-Sills, Yuval Freed, Rami Eliasi, et al. Fracture toughness of the +45°/-45°interface of a laminate composite [J]. Int J Fract, 2006(141): 195-210.
[11]
Hudson Ryan C, Davidson Barry D, Polaha Jonathan J. Effect of remote ply orientation on the perceived mode Ⅰ and mode Ⅱ toughness of θ/θ and θ/-θ interfaces [J]. Applied Composite Materials, 1998(5): 123-138, 1998.
[12]
de Morais A B, de Moura M F, Marques A T, et al. Mode-Ⅰ interlaminar fracture of carbon/epoxy cross-ply composites [J]. Composite Science and Technology, 2002,62(5): 679-686.
