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1·The torsion reduces the effectual attack angle of the elastic sweep wing.

有效迎角的减小又使得弹性机翼的有效气动力载荷减小。

2·With the increase of attack angle, the transiton point moves from the frailing edge to leading edge.

随攻角的增大，转捩点从后沿移向前沿。

3·The yawing can apparently attenuate the angular displacement of both the tail and the attack angle of tail fin.

艏摇的存在会明显的衰减尾柄主臂和尾鳍攻角的角位移。

4·The effect of initial attack angle and pitching angular velocity on the selection of release angle is remarkable.

得到标枪的初始攻角和俯仰角速度对出手角度选择的影响较显著。

5·While for small clearance, there appear repulsion phenomena, and the variation of coefficients with attack Angle is nonlinear.

当物体离壁面很近时，出现排斥现象，水动力系数随攻角的变化呈非线性特征。

6·In this paper wing had wing-blade and wing hadn't wing-blade applied for wind tunnel tests at different attack Angle and velocity.

文中进行了带翼刀机翼和不带翼刀机翼在不同迎角和风速下的风洞吹风试验。

7·When flapping-wing flight at small attack Angle, wing had wing-blade improve effectively aerodynamic characteristic of flapping-wing.

当扑翼在小迎角飞行时，机翼带翼刀可以有效地改善扑翼的气动特性。

8·The optimization of maximum attack Angle is evaluated according to the given initial design parameters by using the orthogonal method.

最大攻角的优化根据给定的初始设计值采用正交法进行。

9·The guidance and control system is properly designed and can meet the accuracy and attack Angle requirement for still or mobile target.

制导控制系统设计合理，对于静止和机动目标，落点射击精度和落角均满足设计要求。

10·This paper presents two methods of using double servo accelerometers to make precision model attack angle measurements in wind tunnel testing.

提出采用双伺服加速度计同轴和垂直系统的两种方法，能够解决风洞模型攻角传感测量中的抗振动干扰问题。