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1)  low incidence
小迎角
2)  angle of attack
迎角
1.
Research on method of angle of attack measurement based on pressure sensors;
基于压力传感器的迎角测量方法的研究
2.
In the condition of gust,in order to restrain additional load and improve the comfort of passenger,the state of angle of attack is acquired.
在阵风条件下,为了抑制飞机的附加载荷并改善乘坐品质,需要得到飞机的迎角状态。
3.
For several reasons, the angle of attack and the sideslip angle cannot be measured accurately especially when angle of attack is high.
针对迎角和侧滑角,特别在大迎角飞行情况下不能够精确测量的问题,研究了一种利用INS/GPS系统数据结合其他辅助系统来估计迎角和侧滑角的方法,利用INS/GPS系统测量的地速和总加速度信号结合飞机其他传感器和数学模型估计得到了迎角和侧滑角传感器的虚拟信号。
3)  angle of attack;incident angle
攻角,迎角
4)  critical angle of attack
临界迎角
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。
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