Citation: | FAN Jin-juan, TAO Chun-hu, ZHANG Bao-cai, ZHAO Xu. Fracture Analysis of Front Edge of Resin Based Carbon Fiber Composite Wainscot[J]. Materials and Mechanical Engineering, 2008, 32(12): 85-87. |
[1] |
Cheng Xiaoquan,Kou Changhe,Li Zhengneng.Compression of composite honeycomb core sandwich panel after low velocity impact[J].Journal of Beijing University of Aeronautics and Astronautics,1998,24(5):551-554.
|
[2] |
Peng Jun,Liu Yanyong.Damage simulation of composite laminated plate subjected to low velocity impact[J].Journal of Northwestern Polytechnical University,2002,20(1):28-31.
|
[3] |
de Freitas M,Reis L.Failure mechanisms on composite specimens subjected to compression after impact[J].Composite Structures,1998,42:365-373.
|
[4] |
Tian Jiong,Sun Yongqi.Direct observation and analysis on the crack tip damage of resin matrix composite[J].Journal of Northwest Institute of Textile Science and Technology,1996,10(1):1-5.
|
[5] |
Clegg R,Hayhurst C,Leahy J,et al.Application of a coupled anisotropic material model to high velocity impact response of composite textile armour[C]// 18th International Symposium on Ballistics San Antonio,TX:[s.n.],1999:11.
|
[6] |
孙聪,王向明.飞机结构典型故障分析与设计改进[M].北京:航空工业出版社,2007.
|