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编织结构复合材料力学性能分析
引用本文:孙慧玉,吴长春,黄传奇.编织结构复合材料力学性能分析[J].航空学报,1997,18(4):458-461.
作者姓名:孙慧玉  吴长春  黄传奇
作者单位:中国科学技术大学力学和机械工程系;南京航空航天大学飞行器系
基金项目:国家自然科学基金,航空科学基金
摘    要:以分析编织结构复合材料的力学性能和修正的经典层合板理论为基础,首先对三维编织织物结构进行分析,考虑厚度方向的效应,采用三维应力-应变分析,预报编织结构复合材料的有效弹性模量;同时,进行了编织结构复合材料的力学性能实验,理论预报和试验结果符合得较好。

关 键 词:复合材料  三维编织  力学性能  
收稿时间:1996-10-10;
修稿时间:1997-03-28

ANALYSIS OF MECHANICAL PROPERTIES OF BRAIDED STRUCTURAL COMPOSITE MATERIALS
Sun Huiyu,Wu Changchun.ANALYSIS OF MECHANICAL PROPERTIES OF BRAIDED STRUCTURAL COMPOSITE MATERIALS[J].Acta Aeronautica et Astronautica Sinica,1997,18(4):458-461.
Authors:Sun Huiyu  Wu Changchun
Institution:Department of Modern Mechanics, University of Science and Technology of China, Hefei, 230026) Huang Chuanqi (Department of Aircraft Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016
Abstract:The mechanical properties of braided structural composite materials are analyzed. The modified classical laminated theory forms the basis of the present approach. Considering the effect of thickness, three dimensional stress strain analysis is adopted. The effective elastic modulus is predicted. In addition, the mechanical experiments of braided structural composite materials are carried out. The theoretical prediction shows reasonably good agreement with the test result.
Keywords:composite materials  three  dimensional braiding  mechanical properties
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