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非对称复合材料结构特性分析及其应用 被引量:3

Analysis and application of unsymmetric composite structure
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摘要 为了解决机翼的扭转发散、载荷重新分布及操纵反效和操纵效率等问题 ,基于非对称复合材料的各向异性及相对于普通复合材料更好的可设计性 ,以几种典型非对称复合材料层板的试验及计算为基础研究了非对称层合板的各种耦合特性 ,并进行了非对称复合材料机翼的设计 ,得到了满意的结果 . Unsymmetric composite structure is a kind of orthotropic material, and has more designabilities than symmetric composite structure. Those abilities can be used to solve such wing's problems in design as twist diversion, redistribution of load and low efficiency of control. Based upon the results of experiment and calculation of several representative unsymmetric composite laminates, the coupling characteristics of unsymmetric laminate was studied. An airplane wing made of unsymmetric composite structures was designed. And good result was got.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2003年第9期770-773,共4页 Journal of Beijing University of Aeronautics and Astronautics
基金 航空科学基金资助项目
关键词 复合材料 耦合 载荷分布 操纵效率 composite materials coupling loads distribution control efficiency
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二级参考文献3

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共引文献3

同被引文献31

  • 1万志强,杨超,郦正能.混合遗传算法在气动弹性多学科优化中的应用[J].北京航空航天大学学报,2004,30(12):1142-1146. 被引量:20
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