航空学报 > 1988, Vol. 9 Issue (2): 11-16

具有机翼和立尾的尖头机身的不对称背涡及其气动特性

陈南茜   

  1. 北京航空学院
  • 收稿日期:1987-04-07 修回日期:1900-01-01 出版日期:1988-02-25 发布日期:1988-02-25

THE CHARACTERISTICS OF ASYMMETRIC VORTICES AND SIDE FORCES ON A SHARP-NOSED BODY WITH WING AND VERTICAL TAIL

Chen Nanqian   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1987-04-07 Revised:1900-01-01 Online:1988-02-25 Published:1988-02-25

摘要: 在低速大迎角无侧滑情况下,翼身组合体(BW),翼身、立尾组合体(BWV)的侧力系数随迎角的变化规律与对应的单独机身的相应特性基本相仿。在有侧滑(|β|≤8°)的情况下,翼身组合体的侧力系数和偏航力矩系数随迎角的变化规律与无侧滑的情况也基本相仿。三种边条对抑制机身的不对称背涡在各种情况下均有显著效果。

Abstract: The variations of side force Cx vs angles of attack a on the wing-body combination and wing-body-vertical tail combination are similar to that on the body alone at high angles of attack with zero side-slip. They are also similar to that of Cz vs a on the wing-body combination at high angles of attack with-8°<β<8°. Three kinds of strakes arc found to be highly effective on alleviating asymmetric vertices, as well as induced side forces on the body, wing-body-vertical tail combinations with zero side-slip and high angles of attack.