tail angle
英 [teɪl ˈæŋɡl]
美 [teɪl ˈæŋɡl]
网络 尾角
双语例句
- Cantilever tail plate: structure more complex load large plate surface angle can be adjusted;
悬臂式尾板：结构较复杂，载重量大，板面角度可调节； - The drag reduction caused by separation weakening on vertical tail results in drag increasing slowly with the increase of the positive attack angle.
垂尾分离随迎角增加而不断减弱，从而导致正常式布局后体阻力随迎角变化表现为非对称。 - 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。 - Research on Library User "Long Tail" in China from an Angle of Humanism Spirits
人文精神视角下我国图书馆用户长尾研究 - The variation of horizontal tail position due to the angle of attack should be taken into account when wall-interference corrections on the longitudinal stability are performed.
对纵向静稳定性作洞壁干扰修正时，应考虑由于攻角改变平尾在风洞实验段中位置的变化。 - The chord-wise location of the vertical tail has little influence on the buffeting onset angle but large influence on the maximum buffeting response intensity;
垂尾弦向位置对垂尾抖振起始迎角影响较小，但对最大抖振响应影响较大； - This paper presents the effect of tail sting and the angle of boat tail on the base pressure at supersonic velocities.
本文介绍了天平尾支杆以及模型船尾对超声这弹丸底压测量影响的实验研究和理论计算。 - Through using multi-frequency theory to analyze the noise of the tail rotor, the relative sound pressure variable law is calculated according to the variation of scissors angle.
本文通过利用多频调制方法对尾桨噪声进行理论分析，得出相对声压值随剪刀变化的规律； - Study on Effect Tail Clearance Angle in NC Sharpening of Twist Drills
钻尖数控刃磨中的尾隙角研究 - Through simulation tail trace of upstream blade end wall by smoke, it summarize sweep effect of blade on smoke flow and the rule of the clearance leakage flow under different speed, the smoke flow diffuser angle decrease and the deflection angle increase as the rotor speed up.
通过烟雾模拟上游叶片端壁尾迹，总结出不同转速下叶片对烟雾流的掠扫效应和间隙泄漏流动的规律，随着转子转速的提高，烟雾流扩散角减小，偏转角增大。 - The location of the center of gravity, the length of the tail, the bend angle and the relationship between each other are discussed and a Variable bend tail vehicle configuration has been presented which has an acceptable hinge moment for a wide range of trimming flight conditions.
通过研究分析飞行器的质心位置、弯尾部分的尾长和弯尾角的相互关系，获得了使铰链力矩在飞行器较大配平范围内保持可接受程度的可变弯尾飞行器气动布局。