期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

悬停状态旋翼流场计算方法评述 被引量：2

TECHNIQUES OF FLOWFIELD OF A HELICOPTER ROTOR IN HOVER,AN OVERVIEW
下载PDF
导出
摘要 对现有的悬停状态直升机旋翼流场研究方法进行了综合评述 ,提出了需要解决的相关问题 。 The techniques of flowfield of a helicopter rotor in hover are reviewed.Correlative problems need to be solved are put forward.Prospects of the technique of flowfield of a helicopter rotor are forecasted.
作者 魏靖彪 薛晓中 舒敬荣 孙传杰
机构地区 南京理工大学动力工程学院
出处 《弹道学报》 CSCD 北大核心 2002年第3期90-96,共7页 Journal of Ballistics
关键词 悬停状态 旋翼流场 计算方法 直升机 flowfield of a helicopter rotor,vortex,CFD
分类号 V211.52 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献34

  • 1Wang Shicun.Generalized Vortex Theory of the Lifting Rotor of Helicopter.AD 286576,1961
  • 2Langdgrebe.An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry Characteristics.AD 728835,1971
  • 3Kocured J D,Tangler J L.A Prescribed Wake Lifting Surface Hover Performance Analysis.Journal of the American Helicopter Society,1997,22(1)
  • 4Clark D R and Leiper A C.The Free Wake Analysis a Method for the Prediction of Helicopter Rover Hovering Performance.Journal of the American Helicopter Society,1970,15(1)
  • 5Sadler S G.Development and Application of a Method for Predicting Rotor Free Wake Position and Resulting Rotor Blade Airloads.NASA-CR-1911,1971
  • 6Bliss D B,Quackenbush T R,Bilanin A J.A New Methodology for Helicopter Free Wake Analysis.39th Annual Forum of the American Helicopter Society,1983
  • 7Bliss D B,Teske M E,Quackenbush T R.Free Wake Calculations Using Curved Vortex Elements.Presented at the International Conference on Rotorcraft Basic Research,1985
  • 8Bliss D B,Wachspress D A,Quackenbush T R.A New Approach to the Free Wake Problemn for Hovering Rotors.41th Annual Forum of the American Helicopter Society,1985
  • 9Bliss D B,Teske M E,Quackenbush T R.A New Methodology for Free Wake Analyses Using Curved Vortex Elements.NASA CR-3958,1987
  • 10Quackenbush T R,Bliss D B,Wachspress D A.Computational Analysis of Hovering Performance Using a New Free Wake Method.Presented at the International Conference on Rotorcraft Basic Research,college Park,MD,1988

同被引文献15

  • 1招启军,徐国华.直升机旋翼下洗流场的数值模拟[J].南京理工大学学报,2005,29(6):669-673. 被引量：5
  • 2于子文,曹义华.前飞旋翼三维湍流场的数值模拟[J].北京航空航天大学学报,2006,32(7):751-755. 被引量：10
  • 3唐正府,张靖周.利用喷管引射和旋翼下洗的红外抑制器特性研究[J].南京航空航天大学学报,2007,39(3):288-292. 被引量：4
  • 4CAO Y H, YUAN K G, LI X Y. Computational methods for simulation of flow around helicopter engine inlet[ J]. Journal of Aircrafi, 2006, 43(1): 141 -146.
  • 5GUPTA V, BAEDER J D . Investigation of quad tiltrotor aerodynamics in forward flight using CFD [ C ]. 20th AIAA Applied Aerodynamics Conference. Missouri: St. Luis, 2002:1-11.
  • 6BALLAND M, VERSEUX O, ESTEVE M J. Aero thermal computations with experimental comparison applied to aircraft engine nacelle compartment [ C ]. Proceedings of GT2005 ASME Turbo Expo 2005 : Power for Land, Sea and Air. USA: Nevada Reno-Tahoe, 2005 : 1217-1225.
  • 7MЛ米里 景山译.直升机计算与设计(第一卷)[M].北京:国防工业出版社,1977..
  • 8Kocured J D, Tangler J L. A prescribed wake lifting surface hover performance analysis[J]. Journal of the American Helicopter Society, 1977,22(1):24～35
  • 9王适存.直升机空气动力学[M].航空专业教材编审组,1985..
  • 10王平,王适存,郭才根.共轴式双旋翼气动特性的固定尾迹分析[J].南京航空航天大学学报,1997,29(6):708-711. 被引量：5

引证文献2

二级引证文献4

弹道学报
2002年 第3期

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