1) aerodynamical characteristics at high angles of attack
大迎角特性
2) high angle of attack aerodynamic characteristics
大迎角气动特性
3) lateral directional aerodynamic characteristics at high angle of attack
大迎角横向气动特性
4) aerodynamics at high angle of attack
大迎角气动性能
5) high angle of attack
大迎角
1.
Investigation on the interference of rear sting supports at high angle of attack in low speed wind-tunnel;
低速大迎角尾撑支架干扰试验研究
2.
Study on high angle of attack test technique of rear sting supports;
尾撑大迎角试验技术研究
3.
Investigation of improving the lateral static stability for the aircraft applied to high-subsonic flow and high angle of attack;
某型飞机高亚声速大迎角横向静稳定性改善研究
6) high angles of attack
大迎角
1.
Primal research of the effect of flow turbulence on aerodynamic characteristics of a aircraft model at high angles of attack;
湍流度对飞行器模型大迎角气动特性影响的初步研究
2.
Effects of grit strip on flow asymmetry over a slender revolution body at high angles of attack;
粗糙带对细长体大迎角流动非对称性的影响
3.
An investigation on the effect of the acoustic excitation on flow asymmetry over a slender revolution body at high angles of attack in compressible flows;
可压缩流中声激励对细长体大迎角流动非对称性的影响研究
补充资料：迎角
又称“攻角”、“冲角”。相对气流方向与翼型或机翼(没有侧滑时)的翼弦的夹角。一般以飞机抬头时的迎角为正。侧滑时，迎角则为飞行速度矢量在飞机对称平面上的投影与飞机纵轴之间的夹角。水平尾翼的升降舵向上或向下偏转时，可改变飞机迎角。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条