A , Van Hemelrijck D, Philippidis T P , Cardon A. Design of a cruciform specimen for biaxial testing of fibre reinforced composite laminates [J]. Composites Science and Technology , 2006, 66(7/8): 964―975.
[2]
M, Van Hengel C, Bosker O J. Static properties of fibre metal laminates [J]. Applied Composite Materials, 2003, 10(4/5): 207―222.
[3]
万敏, 周贤宾. 基于极限应变分析的十字形试件有限元分析[J]. 北京航空航天大学学报, 2001, 27(1): 105―108.[3] Yu Yong, Wan Min, Zhou Xianbin. FEM design of cruciform biaxial tensile specimen based on limit strain analysis [J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 105―108. (in Chinese)
[4]
万敏, 吴向东, 王海波. 中心区减薄的十字形试件拉伸性能研究[J]. 塑性工程学报, 2007, 14(6): 55―58.[4] Han Fei, Wan Min, Wu Xiangdong, Wang Haibo. Investigation of tensile formability of thinned sheet metal and cruciform specimen with thinned central test region [J]. Journal of Plasticity Engineering, 2007, 14(6): 55―58. (in Chinese)
[5]
方如华, 曾伟明, 朱启荣, 朱金龙. 材料的双轴拉伸的规律的研究[J]. 实验力学, 2006, 21(5): 596―600.[5] Yang Guobiao, Fang Ruhua, Zeng Weiming, Zhu Qilong, Zhu Jinlong. Experimental study of spring-back emulation system with high precision [J]. Journal of Experimental Mechanics, 2006, 21(5): 596―600. (in Chinese)
[6]
方岱宁. 功能材料双轴拉伸十字板试件的优化设计[J]. 力学学报, 2002, 34 (5): 705―713.[6] Wang Yinghui, Fang Daining. Optimal design of biaxial tensile cruciform specimens for smart materials [J]. Chinese Journal of Theoretical and Applied Mechanics, 2002, 34(5): 705―713. (in Chinese)
[7]
实用飞机结构工程设计[M]. 北京: 航空工业出报社, 2008: 520―525.[7] Niu Chunyun. Airframe Structural Design [M]. Beijing: Aviation Industry Publishers, 2008: 520―525. (in Chinese)
[8]
C, Filious C, Pateau V. Strength prediction of fiber reinforced plastics with a hole under compression tension [J]. AIAA Journal, 2000, 38(1): 110―114.
[9]
Neill, G S. Asymmetric reinforcements of a quasi-isotropic graphite epoxy plate containing a circular hole [R]. Naval Postgraduate School, Monterey, CA. Jun 1982.207p.
[10]
D H, Sillivan P. Analysis of symmetric reinforcement of quasi-isotropic graphite/epoxy plates with a circular cutout under uniaxial tension loading [R]. Naval Postgraduate School, Monterey, CA. Dec 1983.112p.
[11]
G, Tamara H, Holger O. Application of the tailored fibre placement (TFP) process for a local reinforcement on an “open-hole ” tension plate from carbon/epoxy laminates [J]. Composites Science and Technology, 2003, 63(1): 81―88.
[12]
S, Morishima R, Zhang X. Cutout shape and reinforcement design for composite C-section beams under shear load [J]. Composite Structures, 2009, 88(2): 179―187.
[13]
汪彤, 郦正能, 杨旭. 复合材料层压板开口增强研究[J]. 北京航空航天大学学报, 1997, 23(4): 477―481.[13] Kou Changhe, Wang Tong, Li Zhengneng, Yang Xu. Reinforcement research of composites containing a circular hole [J]. Journal of Beijing University of Aeronautics and Astronautics, 1997, 23(4): 477―481. (in Chinese)
[14]
寇长河, 于卫东, 石天路. 复合材料层合结构开口的非对称增强研究[J]. 航空学报, 1994, 15(12): 1478―1481.[14] Luo Xiaodong, Kou Changhe, Yu Weidong, Shi Tianlu. Asymmetric submerged reinforcement of composite laminates containing a circular hole [J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(12): 1478―1481. (in Chinese)
[15]
J, Loughlan J. The buckling response of carbon fiber composite panels with reinforced cutouts [J]. Composite Structures, 1995, 32(1/2/3/4): 97―113.
[16]
S, Kinloch A J, Matthews F L , Crisfield M A . The mechanical performance of repaired stiffened panels Part I: Experimental characterization [J]. Composites, 2002, 33(5): 343―354.
[17]
S, Kinloch A J, Crisfield M A. The mechanical performance of repaired stiffened panels Part II: Finite element modeling [J]. Composites, 2002, 33(5): 355―366.
[18]
复合材料结构开孔分析第一部分: 板类开孔问题[J]. 导弹与航天运载技术, 1994, (3): 34―46.[18] Wu Delong. Cutout analysis of composite structures part 1:The cutout problems in composites plates [J]. Missiles and Space Vehicles, 1994(3): 34―46. (in Chinese)
[19]
复合料层压板开口的非对称增强研究[J]. 导弹与航天运载技术, 2009(4): 40―43.[19] Shang Lin. Research on asymmetric reinforcement of opening in composite laminate [J]. Missiles and Space Vehicles, 2009(4): 40―43. (in Chinese)
[20]
Onal, Sabit Adaburt. 对二维编织复合材料弹性、热、强度、及失效分析模型的评论[J]. 力学进展, 2008, 38(4): 502―517.[20] Levent Onal, Sabit Adaburt. Modeling of elastic, thermal and strength/failure analysis of two-dimensional woven composites-a review [J]. Advances in Mechanics, 2008, 38(4): 502―517. (in Chinese)
[21]
N K, Tiwari S I, Kumar R S. An analytical model for compressive strength of plain weave fabric composites [J]. Compos Sci Technol, 2003, 63(5): 609―625.
[22]
T,Chou T W. Elastic behavior of woven hybrid composites [J]. Compos Mater, 1982, 16(7): 2―19.
[23]
M, Kurath P. Deformation and failure behavior of woven composite laminates [J]. Journal of Engineering Materials and Technology-Transactions of the ASME, 1994, 116(2): 222―232.
[24]
D, Aboura Z, Benzeggagh M L, Bocherens E. A micromechanics model for 3D elasticity and failure of woven fiber composite materials [J]. Composites Science and Techonlogy, 1999, 59(4): 505―517.
[25]
许希武, 郭树. 二维二轴1×1编织复合材料细观结构模型及力学性能有限元分析[J]. 复合材料学报, 2011, 28(6): 215―222.[25] Zhang Chao, Xu Xiwu, Guo Shu. Microsture model and finite element analysis of mechanical properties of 2D 1×1 biaxial braided composites [J]. Acta Materiae Compositae Sinica, 2011, 28(6): 215―222. (in Chinese)
[26]
Z. Failure criteria for unidirectional fiber composites [J]. Journal of Applied Mechanics, 1980, 47(2): 329―334.
