1.
curve of moment against incidence
力矩与迎角的关系曲线
2.
The conventional tail must be at a negative angle of attack, and the Canard tail at a positive angle.
通常的尾翼必须处于负迎角，而鸭式尾翼则为正迎角。
3.
The velocity distributions previously shown were for a single angle of attack.
先前的速度分布列分别为单一迎角.
4.
NUMERICAL STUDY ON THE SLENDER BODY AT HIGH ANGLE OF ATTACK
细长旋成体大迎角分离控制数值研究
5.
The development of high angle of attack test equipment in the 8m×6m low speed wind tunnel
8m×6m风洞特大迎角试验设备研制
6.
Pressure Distribution Characteristics around a Slender Circular Cone at 35° Angle of Attack and Low Speed
20°圆锥低速35°迎角下的压力分布特性
7.
Numerical Investigation of Unsteady Aerodynamic Characterisics of Pitching Delta Wings
三角翼大迎角俯仰运动气动特性数值研究
8.
Frequency characteristics of breakdown vortices over delta wings with small amplitude oscillation at the high angle of attack
大迎角下小振幅振荡三角翼破裂涡的频率特性
9.
so does the ratio of lift anddrag, it gains only with the increase of the angle of release and goes to the maximum when the release angle is 25°.
升阻比和出手初速关系不大,它随迎角的加大而增大,迎角25°时达最大值。
10.
Effects of Vortex Generators on Maximum Lift and Stall Angle of Attack over Wings
旋涡发生器对机翼最大升力和失速迎角的影响
11.
Experimental investigation on pressure distribution characteristics of wings of ×× missile at supersonic speeds and high angles of attack
××导弹翼面超声速大迎角压力分布特性试验研究
12.
MULTIPLE LINE-VORTEX MODEL OF VORTEX FLOWS AROUND BODY OF REVOLUTION AT HIGH ANGLES OF ATTACK UP TO 60 DEGREES
迎角直到60度旋转体涡流的多重线涡模型
13.
Nonlinear Dynamic Characteristics Analysis and Control of Aircraft at High-Angle-of-Attack;
飞机大迎角非线性动力学特性分析与控制
14.
The Research on the Method of Angle of Attack Measuring Based on Four-Quad Pressure Sensors;
基于四象限压力传感器的迎角测量方法研究
15.
An Analysis of Trimming Regularity of the Best Wind Angle for International 470 Class Yacht;
国际470级帆船最佳迎角的调整规律分析
16.
Computation of Vehicle Pitching Static and Dynamic Derivatives at High Angles of Attack
飞行器大迎角下俯仰静、动导数的数值计算
17.
Signal Preprocessing of Angle of Attack Sensor Based on Wavelet Analysis
基于小波分析的迎角传感器信号预处理
18.
A High Angle of Attack Dynamical System Identification Algorithm Based on LS-SVM
基于LS-SVM飞机大迎角动态辨识方法研究