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相关技术

螺旋桨和弹载无人机相互干扰分析

  • 宋琦 ,
  • 李勇 ,
  • 杨树兴 ,
  • 王飞 ,
  • 姚伟
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  • 1 中国空间技术研究院,北京 100094
    2 北京理工大学,北京 100081

宋琦(1979-),男,湖北人,工程师,研究方向:飞行器设计。

收稿日期: 2010-03-29

  网络出版日期: 2025-05-30

Airflow Interference Analysis between Propeller and UAV

  • SONG Qi ,
  • LI Yong ,
  • YANG Shuxing ,
  • WANG Fei ,
  • YAO Wei
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  • 1 China Academy of Space Technology, Beijing 100094, China
    2 Beijing Institute of Technology, Beijing 100081, China

Received date: 2010-03-29

  Online published: 2025-05-30

摘要

为了研究螺旋桨与弹载无人机的相互干扰,使用滑移动网格技术对螺旋桨进行数值仿真,借助颗粒轨迹、分段受力计算和相关力矩计算对仿真结果进行分析。分析结果表明螺旋桨的干扰会对无人机稳定性产生影响,借助副翼偏转和垂尾的恢复力矩可以使无人机保持相对稳定;螺旋桨的滑流掠过机翼使升力增加,并产生与螺旋桨扭矩相反的力矩。

本文引用格式

宋琦 , 李勇 , 杨树兴 , 王飞 , 姚伟 . 螺旋桨和弹载无人机相互干扰分析[J]. 弹箭与制导学报, 2011 , 31(1) : 211 -214,218 . DOI: 10.15892/j.cnki.djzdxb.2011.01.068

Abstract

The slide mesh technology has been used for the objective that the interference between propeller and UAV is researched through numerical simulation. In the process of analyse, the method of the particle track, part of force and statistic of moment has been done. The result shows that UAV can keep relatively stable by aileron and vertical tail. The propeller slipstream has some effect to UAV, such as the increase of life in the wing and reversed torque of propeller.

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参考文献

[1]
Rruno J C, Barth T J.Numerical simulation of unsteady Euler flow around multibladed rotor in forward flight using a moving grid approach [C]// Proceedings of 51st Annual Forum of AHS, 1995.
[2]
Liu C H, Thomas J L, Tung C.Navier-Stokes calculations for the wake of a rotor in hover.AIAA-83-1676[R].1983.
[3]
Nathan Hariharan, L N Sankar, J Russell, et al. Numerical simulation of rotor airframe interaction[C]// 33rd Aerospace Sciences Meeting and Exhibit, Reno Hilton, January 9-12, 1995.
[4]
王立群, 乔志德, 张茹. 基于动态网格的旋翼流场计算[J]. 计算物理, 2000, 17(4): 367-371.
[5]
白俊强, 刘千刚. 直升机旋翼非定常气动力及结构动力响应计算[J]. 飞行力学, 1998, 16(1): 32-36.
[6]
许和勇. 基于动态对接网格的非定常流动计算方法研究[D]. 西安: 西北工业大学, 2006.
[7]
宋琦、 杨树兴, 徐勇, 等. 滚转状态下卷弧翼火箭弹气动特性的数值模拟[J]. 固体火箭技术, 2008, 31(6): 552-554.
[8]
Jin Zhu, Ted Blacker, Rich S. Background overlay grid size functions[C]// Proceedings 11th International Meshing Roundtable, Sandia National Laboratories, 2002: 65-74.
[9]
Eric L Blades David L Marcum. A sliding interface method for unsteady unstructured flow simulations[J]. International Journal for Numerical Methods in Fluids, 2007, 53(3): 507-529.
[10]
朱自强. 应用计算流体力学[M]. 北京: 北京航空航天大学出版社, 1998.
[11]
陶文铨. 数值传热学[M]. 西安: 西安交通大学出版社, 2001.
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