杜善义, 关志东. 我国大型客机先进复合材料应对策略思考 [J]. 复合材料学报, 2008, 25(1): 1-10. Du Shanyi, Guan Zhidong. Strategic considerations for development of advanced composite technology for large commercial aircraft in China [J]. Acta Materiae Compositae Sinica, 2008, 25(1): 1-10.
[2]
Armstrong K B, Bevan L G, Cole II W F. Care and repair of advanced composites [M]. 2nd edition. Warrendale, PA USA: SAE International, 2005: 263-265.
[3]
Jones J S, Graves S R. Repair techniques for Celion-LARC-160 graphite-polyimide composite structures . Washington: NASA, 1984.
Kumar S B, Sridhar I, Sivashanker S I, et al. Tensile failure of adhesively bonded CFRP composites scarf joints [J]. Materials Science and Engineering B, 2006, 132(1/2): 113-120.
[6]
Kumar S B, Sivashanker S I, Osiyemi S O, et al. Failure of aerospace composite scarf-joints subjected to uniaxial compression [J]. Materials Science and Engineering A, 2005, 412(1/2): 117-122.
[7]
Pipes R B, Adkins D W, Deaton J. Strength and repair of bonded scarf joints for repair of composite materials . Washington: NASA, 1982.
[8]
Odi R A, Friend C M. An improved 2D model for bonded composite joints [J]. International Journal of Adhesion & Adhesives, 2004, 24(5): 389-405.
[9]
Campilho R D S G, Moura M F S F, Domingues J J M S. Stress and failure analyses of scarf repaired CFRP laminates using a cohesive damage mode [J]. Journal of Adhesion Science and Technology, 2007, 21(9): 855-870.
[10]
Wang C H, Gunnion A J. On the design methodology of scarf repair to composite laminates [J]. Composite Science and Technology, 2008, 68(1): 35-46.
[11]
Boeing Ltd. Boeing 737-800 structural repair manual [S]. USA: Boeing Ltd. 2003.
[12]
Airbus Ltd. Airbus A320 structural repair manual [S]. France: Airbus Ltd. 2007.
[13]
邹 健, 程小全, 邵世刚, 等. 基于ANSYS环境的平面编织层合板拉伸破坏数值仿真 [J]. 复合材料学报, 2007, 24(6): 180-184. Zou Jian, Cheng Xiaoquan, Shao Shigang, et al. Numerical simulation for plain woven composite laminate based on ANSYS software [J]. Acta Materiae Compositae Sinica, 2007, 24(6): 180-184.
[14]
程小全, 邹 健, 许延敏, 等. 含孔平面编织混杂铺层层合板压缩破坏仿真 [J]. 力学学报, 2007, 39(6): 829-834. Cheng Xiaoquan, Zou Jian, Xu Yanmin, et al. Simulation of compressive failure of hybrid plain woven fabric laminate with a hole [J]. Chinese Journal of Theoretical Applied Mechanics, 2007, 39(6): 829-834.
[15]
Hashin Z. Failure criteria for unidirectional fiber composites [J]. Journal of Applied Mechanics, 1980, 47(2): 329-334.
[16]
许延敏. 平面编织复合材料层压板拉压性能研究 . 北京: 北京航空航天大学, 2007. Xu Yanmin. Investigation on tensile and compressive properties of plain woven laminates . Beijing: Beihang University, 2007.
[17]
郑海燕. 编织复合材料的低速冲击及冲击后压缩特性研究: 试验及数值计算 . 西安: 西北工业大学, 2002. Zheng Haiyan. Study on low velocity impact and compressive characteristic after impact of woven composites: Testing and numerical estimate . Xi’an: Northwestern Polytechnical University, 2002.
[18]
Camanho P P, Davila C G. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials . Washington: NASA, 2002.
[19]
Turon A, Davila C G, Camanho P P, et al. An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models [J]. Engineering Fracture Mechanics, 2007, 74(10): 1665-1682.
[20]
Wang C H, Gunnion A J. Design methodology for scarf repair to composite structures . Melbourne: Defense Science and Technology Organization, 2006.
[21]
Gunnion A J, Herszberg I. Parametric study of scarf joints in composite structures [J]. Composite Structures, 2006, 75(1-4): 364-376.
