attack angle的例句大全

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

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

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

Study of locomotive wheel-rail attack angle testing system

机车轮轨冲角测试系统研究

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

Control law study of aircraft maneuvers at high attack angle

飞机大迎角机动飞行控制律研究

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

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。

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

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

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。

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。

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。

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。

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.

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.

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.

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.

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.

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.