CHEN Guo-tao, MEI Zhi-yuan, LI Hua-dong. THE EXPERIMENTAL RESEARCH FOR DESIGN ALLOWABLE OF TENSION STRENGTH OF SW220/430LV COMPOSITE MATERIAL[J]. COMPOSITES SCIENCE AND ENGINEERING, 2015, 0(9): 11-16.
[1] 沈真, 张晓晶. 复合材料飞机结构强度设计与验证概论. 上海: 上海交通大学出版社, 2011.1-11.
[2] R.A.SHENIO, J.F.WELLICOME.Composite Materials in Maritime Structures. Cambridge University Press, 1993, 3-4: 179-197.
[3] Department of Defence. Polymer Matrix Composites Guidelines for Characteristic of Structural Materials. United States of America:
[4] 2002.
[5] 欧阳吕伟, 吴剑国. 基于可靠性的潜艇结构安全系数研究总结报告. 2005.
[6] 沈真. 复合材料结构设计手册. 北京: 航空工业出版社,
[7] 2001.
[8] 刘文珽. 结构可靠性设计手册. 北京: 国防工业出版社, 2008. 143-200.
[9] Abouelheiga M. Component Design for Automated Aircraft Composite Structure Manufacture .2010.
[10] 徐孝诚. 复合材料结构强度散布特性及可靠性问题的讨论. 强度与环境, 1991, 25-29.
[11] Wang C H, Miller K J. Short fatigue crack growth under mean stress, uniaxial loading. Fatigue and Fracture of Materials and Structures, 1993,16(2): 181-198.
[12] Du Quesnay D L, Topper T H, et al. The effect of notch radius on the fatigue notch factor and the propagation of short cracks. London: M.E.P, 1986. 323-335.
[13] Miller K J. The behavior of short fatigue cracks and their initiation Part Ⅰ-A review of two recent books. Fatigue and Fracture of Materials and Structures, 1993, 16(2): 181-198.
[14] Seneviratne W. fatigue-Life Determination of Damage-Tolerant Composite airframe.Wichita State University, 2008.
[15] 翟洪军, 姚卫星. 纤维增强树脂基复合材料的疲劳剩余刚度研究进展. 力学进展, 2002, 32(1): 69-80.
[16] 刘鸿文. 材料力学. 北京: 高等教育出版社, 2004.
[17] 崔志华. 复合材料层压板的疲劳特性. 北京: 教育科学出版社, 1996.
[18] 姚卫星. 结构疲劳寿命分析. 北京: 航空工业出版社, 2003.