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头部旋转对细长体大迎角不对称涡系影响机理的实验研究
引用本文:苏玳,汪子兴.头部旋转对细长体大迎角不对称涡系影响机理的实验研究[J].空气动力学学报,1988(1).
作者姓名:苏玳  汪子兴
作者单位:华东工学院 (苏玳),南京航空学院(汪子兴)
摘    要:本文介绍了头部旋转对大迎角不对称涡系影响的观测结果,说明了由此而抑制大迎角不对称涡系的机理。 实验结果表明,头部旋转对细长体无侧滑大迎角不对称涡系涡迹的影响是:随头部的逐渐转动,涡系的不对称发生了周期性变化;此时,由于涡不可能迅速改变状态,从而抑制、甚至接近消除了大迎角时出现的涡系不对称现象。

关 键 词:旋涡流动  空间涡系  大迎角空气动力学  细长体

EXPERIMENTAL INVESTIGATION ON THE FORMATION MECHANISM OF THE EFFECT OF SPIN NOSE TO ASYMMETRIC VORTEXES ON SLENDER BODY AT HIGH ANGLE OF ATTACK
Su Dai.EXPERIMENTAL INVESTIGATION ON THE FORMATION MECHANISM OF THE EFFECT OF SPIN NOSE TO ASYMMETRIC VORTEXES ON SLENDER BODY AT HIGH ANGLE OF ATTACK[J].Acta Aerodynamica Sinica,1988(1).
Authors:Su Dai
Institution:Su Dai (East China Institute of Technology)Wang Zixing (Nanjing Aeronautical institute)
Abstract:Experimental results of spin nose of a slender body at high angle of attack are presented,and the formation mechanism of the spatial vortexes are also explained in this paper.Experimental results show that the vortex cannot be changed rapidly with the nose spin rate,therefore the asymmetric vortexes on slender body at high angle of attack can be inhibited and approach to vanished.
Keywords:vortex flow  spatial vortex  aerodynamics at high angle of attack  slender body  
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