期刊文献+

直升机旋翼动力学优化浅析 被引量:4

Analysis of Helicopter Rotor Dynamic Optimization
下载PDF
导出
摘要 阐述了直升机旋翼动力学优化在国内外研究发展情况。通过对国内外旋翼动力学模型、优化方法及优化策略等方面的对比研究,得出国内在直升机旋翼动力学优化方面与国外研究的差距,为进一步开展相关优化研究指明了方向。 This paper describes the research and development of helicopter rotor dynamic optimization at home and abroad. Through the comparative study of rotor dynamics models,optimization methods and optimization strategies at home and abroad,we get the gap between domestic helicopter rotor dynamics optimization and foreign research,and point out the direction for further optimization research.
出处 《兵器装备工程学报》 CAS 北大核心 2018年第1期25-28,共4页 Journal of Ordnance Equipment Engineering
基金 中央高校基本科研业务费专项基金项目 国家级大学生创新性实验计划项目
关键词 旋翼气弹动力学 多目标优化 有限元模型 优化方法 优化策略 rotor aeroelastic dynamics multi-objective optimization finite element model optimizationmethod optimization strategy
  • 相关文献

参考文献7

二级参考文献43

  • 1向锦武,张呈林,王适存.低振动旋翼桨叶的动力学优化设计[J].航空动力学报,1996,11(2):125-128. 被引量:13
  • 2刘守慎.低振动旋翼桨叶优化设计方法研究的若干问题[J].第八届全国直升机年会论文集,1992,.
  • 3Ganguli R, Chopra I. Aeroelastic optimization of a helicopter rotor to reduce vibration and dynamic stresses[J]. Journal of Aircraft, 1996,12 (4): 808- 815.
  • 4Gandhi F,Nissly A. Design optimization of a controllable camber rotor airfoil[C]//American Helicopter Society 61st Annual Forum. Grapevine: TX, 2005: 322-331.
  • 5Guo Junxian,Xiang Jinwu. Composite rotor blade design optimization for vibration reduction with aeroelastie constraints chinese[J].Journal of Aeronautics, 2004, 17(3):152-158.
  • 6User's Guide. ISIGHT's optimization techniques [M]. Beijing: SIGHTNA Technologies Co. ,Ltd, 2005.
  • 7Johnson W. Helicopter Theory [M]. Princeton: Princeton University Press, 1980.
  • 8Sobieszczanski-Sobieski J. On the sensitivity of complex internally coupled systems [R]. NASA TM 100537, 1988.
  • 9Chattopadhyay A. Minimum weight design of rectangular and tapered helicopter rotor blades with frequency constraints[R]. NASA Technical Memorandum 100561,1988.
  • 10Chattopadhyay A, Walsh J L, Riley M F. Integrated aerodynamic/dynamic optimization of helicopter rotor blades [R]. Washington, DC: National Aeronautics and Space Administration, 20546-0001, 1989.

共引文献48

同被引文献26

引证文献4

二级引证文献14

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部