Volume 30 Issue 01
Jan.  2004
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Deng Yanmin, Hu Jizhong. Wind tunnel experimental study of aerodynamic interactions between a rotor and a body of a co-axial helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(01): 1-4. (in Chinese)
Citation: Deng Yanmin, Hu Jizhong. Wind tunnel experimental study of aerodynamic interactions between a rotor and a body of a co-axial helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(01): 1-4. (in Chinese)

Wind tunnel experimental study of aerodynamic interactions between a rotor and a body of a co-axial helicopter

  • Received Date: 10 Sep 2002
  • Publish Date: 31 Jan 2004
  • The results of rotors/fuselage aerodynamic interactions for the coaxial helicopter in hovering and forward flight were presented according wind-tunnel experiment. The presence of the rotor wake creates a significant down load on the fuselage which decreases with increasing advance ratio. The interactions above decreased in forward flight, but yaw moment was generated by fuselage; The interaction of coaxial rotors to fuselage changes when the tail plane area, and lower rotor pitch or advance ratio was changed. The interaction of fuselage to coaxial rotors is different from that of single rotor helicopter, such as: in hovering state, the coaxial helicopter fuselage has no obvious effect on rotors, the fuselage generates beneficial interaction to coaxial rotors when in forward flight and the interaction decreases as the advance ratio increases.

     

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  • [1] alch D T. Experimental study of main rotor tail rotor airframe interaction in hover . The 39th Annual Forum of the American Helicopter Scociety . Missouri, 1983 [2] Leihman N B J G, Samak D K, Green M. Investigation of aerodynamic interaction between a rotor and a fuselage in forward flight .The 45th Annual Form of the American Helicopter Society . Boston,1989 [3] Crouse G L, Leishman J G. Interactional aerodynamic in hover and forward flight . The 48th Annual of the American Helicopter Society . Washington, D C, 1992 [4] Coleman C P. A survey of theoretical and experimental coaxial rotor aerodynamic research . NASA Technical Paper 3765, USA,1997 [5] 高 正. 直升机空气动力学的新成果[M]. 北京:航空工业出版社,1999 Gao Zheng. Recent achievements in the field of helicopter aerodynamics [M]. Beijing:Aeronautics Industry Press,1999(in Chinese) [6] 童自力,孙 茂. 共轴式双旋翼流动的N-S方程模拟 . 第13届全国直升机年会学术论文集 . 九江,1997 Tong Zili, Sun Mao. N-S equation simulation of coaxial rotor flow . Annual Forum of the 13th Chinese Helicopter Society . Jiujiang, 1997(in Chinese)
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