期刊文献+

直升机空中共振安全边界预报与验证 被引量:1

Prediction and Verification of Helicopter Air Resonance Safety Envelope
下载PDF
导出
摘要 简略介绍了直升机空中共振建模思路,通过算例计算研究了确定直升机空中共振安全边界的分析技术,讨论了空中共振飞行试验验证方法。为更准确地预计空中共振安全边界,提出了需要进一步研究的内容和考虑的因素。最后,展望了空中共振分析方法的发展方向。 The modeling consideration of helicopter air resonance was introduced simply, the analy- sis technique of determining helicopter air resonance safety envelope was studied through calculation examples, and verification method of air resonance through flight test was discussed in this paper. In order to predict safety envlope more cxactly. further reaserch contents and factors need to consider were suggested. Finally it was looked into the furture devlopement of air resonance analysis tech-nique.
出处 《直升机技术》 2013年第2期1-7,共7页 Helicopter Technique
关键词 空中共振 安全边界 预报 飞行验证 air resonance safety envelope prediction flight test verification.
  • 相关文献

参考文献6

  • 1Hoges D H. Aermechanical Stability of Helicopter with bearingless Main Rotor[ R]. NASA TM - 78459, 1978.
  • 2中国直升机设计研究所,编译.先进无轴承旋翼译文集[Z].中国直升机设计研究所,1997.
  • 3Panda B, Chopra I.. Dynamic Stability of Hingeless and Bearingless Rotors in Forward Flight[ J]. Computers and Mathematics, 1986,12( 1 ).
  • 4Panda B, Mychalowycz E, Kothmann B, et al. Active Controller for Comanche Air Resonance Stability Augmen- tation[ C ]. American Helicopter Society 60TH Annual Forum, 2004.
  • 5Hoges D H, Dowell E H. Nonlinear Equation of Motion for Elastic Bending and Torsion of Twisted Non - uniform Blades [ R]. NASA TND - 7818, 1974.
  • 6Hoges D H, Ormiston R A, Peters D A. On the Nonlinear Deformation Geometry of Euler - Bernoulli Beams [ R ]. NASA TP 1566, 1980.

同被引文献9

引证文献1

二级引证文献1

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