[1] 王汝敏,郑水蓉,郑亚萍. 聚合物基复合材料及工艺[M]. 北京: 科学出版社, 2004. [2] Standard Tests for Toughened Resin Composite: NASA RP 1092-1983[S]. [3] Composite Aircraft Structure (AC20-107A)[Z]. Federal Aviation Administration, 1984. [4] 高峰, 矫桂琼, 高艳秋. 层间颗粒增韧HT3/QY8911的损伤阻抗和损伤容限[J]. 复合材料学报, 2006, 23(1): 167-172. [5] 王仁鹏, 陈普会, 沈真. 准静态压痕力作用下复合材料层压板的损伤阻抗分析[J]. 复合材料学报, 2008, 25(3): 149-153. [6] Dost E F, Avery W B, Finn L B, et al. Impact Damage Resistance of Composite Fuselage Structure, Part 3[C]//Paper Presented at Fourth ACT Conference. 1993. [7] 郑晓霞, 郑锡涛, 沈真, 等. 低速冲击与准静态压痕力下复合材料层合板的损伤等效性[J]. 航空学报, 2010, 31(5): 928-932. [8] 王璐璐, 关志东. 复合材料层板静压入破坏机制[J]. 复合材料学报, 2007, 24(6): 135-139. [9] Yan L, An X F, Yi X S. Comparison with low-velocity impact and quasi-static indentation testing of foam core sandwich composites[J]. International Journal of Applied Physics and Mathematics, 2012, 2(1): 58-62. [10] 刘凤楠, 赵美英, 郭葳. 复合材料层合板准静态压痕损伤分析[J]. 机械科学与技术, 2011, 30(5): 804-812. [11] 罗靓, 张佐光, 李敏, 等. 复合材料层合板准静态压痕实验研究[J]. 复合材料学报, 2007, 24(3): 154-159. [12] 张海清, 周仕刚, 宫占锋, 等. 复合材料层合板静压痕试验及全过程数值分析[J]. 玻璃钢/复合材料, 2014(11): 5-10. [13] 黄发荣, 周燕, 等. 先进数值基复合材料[M]. 北京: 化学工业出版社, 2008. [14] Standard test method for measuring the damage resistance of a fiber-reinforced polymer-matrix composite to a concentrated quasi-static indentation force: ASTM Standard D6264/D6264M-2007[S]. [15] Standard test method for compressive residual strength properties of damaged polymer matrix composite plates: ASTM Standard D7137/D7137M-2007[S]. |