节点文献

导弹升力面扭片刚度衰减研究

Research on stiffness attenuation for torsion slip of missile wing

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 陈晓岚

【Author】 CHEN Xiao-lan(The Second System Design Department of the Second Research Academy of CASIC,Beijing 100854,China)

【机构】 中国航天科工集团公司二院二部 北京100854

【摘要】 针对导弹长期储存升力面扭片刚度衰减问题,用损伤力学的方法给出了扭转力矩随时间变化的解析解,并对解析解进行了数值模拟。结果表明,刚度衰减主要发生在开始阶段,因此研制阶段扭片储存试验不需要太长的时间。

【Abstract】 To solve the problem of stiffness attenuation of torsion slip in view of missile long time storage,the theoretical model which the variety of torsion moment vs time are obtained by using damage mechanics method,at the same time the theoretical model were simulated by numerical method.It is indicated that the stiffness attenuation mainly occures in the beginning stage and the experimentation of torsion slip storage in research and development stage need not cost a long time.

【关键词】 扭片刚度衰减扭矩
【Key words】 Torsion slipStiffness attenuationTorque
  • 【文献出处】 现代防御技术 ,Modern Defense Technology , 编辑部邮箱 ,2005年01期
  • 【分类号】TJ760
  • 【被引频次】1
  • 【下载频次】43
节点文献中: