1、

Measuring the attack angle of insect wings in free-flight

昆虫自由飞行时翅膀攻角的光学测量

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2、

Bracing System for Dynamic Derivative of Large Attack Angle

大攻角动导数支撑系统的设计与研究

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3、

Numerical Study of Attack Angle Characteristics for Integrated Hypersonic Vehicle

一体化高超声速飞行器攻角特性的数值研究

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4、

Study of locomotive wheel-rail attack angle testing system

机车轮轨冲角测试系统研究

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5、

Optimum design and analysis of a centrifugal compressor with large attack angle

大攻角离心压气机优化设计与分析

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6、

Control law study of aircraft maneuvers at high attack angle

飞机大迎角机动飞行控制律研究

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7、

Application of Quantitative Feedback Theory to Attack Angle Robust Control System of Missile

数量反馈理论在导弹攻角鲁棒控制系统中的应用

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8、

Attack Angle can significantly change the flow field of symmetry.

攻角能够明显改变流场的轴对称性。

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9、

Influence of Attack Angle and Lateral Force on the wheel Flange wear of Locomotive

冲角和横向力对机车轮缘磨损的影响

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10、

The Design for Autopilot of Large Attack Angle Missile by Using Feedback Linearization Method

大攻角飞行导弹自动驾驶仪反馈线性化设计

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11、

The model of reentry trajectory is established and the angle of attack is regarded as control variable.

首先建立了高超声速导弹再入段弹道模型,并将攻角作为控制变量。

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12、

The results show that the abrasion of coatings was influenced by many factors, such as attack angle, impact speed, and abradant dosage etc.

结果表明:涂层的冲蚀磨损受到攻角、冲速、磨料量等多种因素的影响。

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13、

The air resistance of damper of 1-dimension trajectory correcting fuses ( 1-D TCF) is measured under pill angle of attack and low wind speed.

一维弹道修正引信阻力器空气阻力的简捷测量,是在弹丸零攻角、低风速下测量空气阻力的试验方法。

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14、

The longitudinal and lateral aerodynamic characteristics of tactical missiles for the conventional and canard configuration can be calculated using this method at Mach number range from 0 to 3.5, angle of attack and yawing angle from 0 to 20 degrees.

本方法可用于计算来流马赫数为0到3.5左右、攻角和侧滑角为0°到20°左右、正常式或鸭式布局的战术弹纵、横向气动力系数。

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15、

The angle of attack of the high-aspect-ratio wings varies largely as the airflow rounds the airfoil.

在飞行状态下气流绕过翼型时,大展弦比机翼的迎角变化范围非常大.

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16、

Angle of attack typically ranges from 3 o to 12 o for a paraglider.

典型的飞行伞攻角范围由3度到12度之间.

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17、

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.

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18、

The existence of angle of attack reduces the inlet performance.

攻角的存在也在一定程度上降低了进气道性能.

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19、

The static aerodynamic characteristics for slender bodies at large angle of attack was analyzed.

研究分析了细长旋成体弹身类型气动外形的大攻角范围气动特性.

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20、

The measurement of the model angle of attack is a key part in wind tunnel test.

模型迎角的测量是风洞试验中非常重要的环节.

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