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• Angle of attack decreases with increasing speed.

增加速度

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• Angle of attack measuring has very important meaning.

测量具有十分重要意义

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• Instead of giving up, Mr Obama needs to change his Angle of attack.

取代放弃巴马需要改变“攻击”角度

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• The aerodynamic drag and lift of javelin increase with angle of attack.

标枪的气动阻力升力随迎增加而增加

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• As seen above the design Angle of attack for the second segment is10deg.

如上所述，设计第二部分是10甘醇。

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• As seen above, the design Angle of attack for the second segment is10 deg.

如上所述，设计第二部分是10甘醇

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• This occurs at one angle of attack for the same wing loading of a paraglider.

这种情形会发生于飞行负载相当于时。

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• The velocity distributions previously shown were for a single Angle of attack.

先前速度分布分别单一

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• For this Angle of attack the corresponding velocity distribution is constant for the second segment.

这个迎角相应速度分布固定第二部分

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• The Angle of attack, pitch Angle and velocity at shifted point for typical trajectory were calculated.

给出了两种控制方法导引律，计算典型弹道俯仰角交班速度等参数。

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• Angle of attack and nose shape of bodies are key factors that asymmetric vortex occurs over slender bodies.

成体的外形，尤其是头部几何形状细长前体出现对称涡的关键因素

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• The influence of the instantaneous angle of attack and ST on the performance of propulsion is investigated.

探讨了水翼瞬时柔度摆动水翼推进性能影响

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• The influence on flow structure and aerodynamic of a slender by sweep wing at high Angle of attack was studied.

研究迎角下，后掠长体绕结构和气动力特性的影响

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• The extended linearization of nonlinear systems is used to design flight control systems at high angle of attack.

利用非线性系统扩展线性化方法设计具有大迎非线性飞行控制系统。

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• Angle of ATTACK, the Angle of the wing chord in relation to the free stream airflow as it moves forward through the air.

，机翼翼在空气向前运动时与自由气流之间夹角。

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• When confronted momentarily with an ascending air current, the paraglider climbs since the Angle of attack has increased.

我们遇到暂时性上升空气时，飞行伞会随著增加而上升

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• In flight, the Angle of attack can only be adjusted to a small degree, as the wing is highly pliable and subject to collapse.

飞行时翼变极度容易折湾及崩溃时，只能调整一个非常小角度。

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• If you were a marketing manager, return to the job with a new Angle of attack that can help make the company more competitive.

如果是个市场拓展经理新的行销理念重回以前岗位可能有助于提升公司的竞争力。

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• The aerodynamic drag of different models at zero angle of attack in the experiment is calculated using the simplified procedure.

攻角实验不同模型空气动力阻力采用简化方法来计算的；

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• The influence of nodal points interval of angle of attack and order of spline function on estimation results is also researched.

同时研究了迎角节点间隔样条函数次数估计结果影响

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• The fore-body with sharp section angle can produce direction stability at middle-higher angle of attack in the case of side-slip.

侧滑时，侧缘的非圆截面机身头部中等和大迎下，具有方向稳定性

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• Another potential advantage results from the fact that the plane is already tilted to a large Angle of attack as it rolls down the runway.

另一个潜在优点飞机跑道滑行时，机翼已经较大迎角

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• 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.

阵风条件为了抑制飞机的附加载荷改善乘坐品质，需要得到飞机迎角状态

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• A simple nonlinear wing theory for the low-aspect-ratio rectangular flat plate with large Angle of attack in incompressible flow is developed.

本文系不可压缩流体大冲小展弦比矩形平板机翼提出—简单非线性理论

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• DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.

介绍DMC - PID串级控制技术应用到无人机无动力飞行时的自动着陆阶段迎角自动控制系统

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• Dynamic aerodynamics characteristic is one of very important parameters of modern maneuverable aircraft to be scaled at high Angle of attack and high speed.

高速大迎动态气动特性衡量新机动飞行器性能重要参数之一。

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• In the experiment for measuring bullet attitude, this measurement system can accomplish real-time measuring small bullet Angle of attack and velocity parameter.

实际弹丸飞行姿态测试试验中，测试系统可以较好的完成实时测试弹丸速度参数的任务。

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• Complex wave structures of supersonic inlet at different Angle of attack and spinning velocity related to high speed spinning and critical status were achieved.

得到高速旋转工况下对应不同旋转角速度，临界工况时，超声速进气道内外流场复杂系结构

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• Complex wave structures of supersonic inlet at different Angle of attack and spinning velocity related to high speed spinning and critical status were achieved.

得到高速旋转工况下对应不同旋转角速度，临界工况时，超声速进气道内外流场复杂系结构

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