aerodynamic的例句大全

Metal powder folw meter The Aerodynamic Simulation of External Flow Field of Terminal Segment of Terminal Homing Projectile

金属粉末流动性测定仪末制导炮弹末制导段外流场气动仿真

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As well, due to the high terminal velocity, the aerodynamic drag penalty would be particularly great.

同时，由于高终端速度，气动阻力的刑罚将是特别大。

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Finally nonlinear six-degree-of freedom simulations of one aerodynamic missile were done, from the results it can be seen that the missile can follow the terrain configuration accurately, and the simulation results also showed that the designed system had strong robustness and rapidly tracking capability.

最后以飞航导弹非线性模型进行6DOF仿真，可以看出导弹能够准确跟踪地形轮廓飞行，仿真结果表明所设计的地形跟踪控制系统具有较强的鲁棒性和快速跟踪性。

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Experimental Study of Aerodynamic Characteristics in a W-shaped Flame Boiler Equipped with a Bin and Feeder System and Fed Tertiary Hot Air in the Boiler Furnace

中储式热风送粉W型火焰锅炉炉内空气动力场实验研究

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A wind tunnel test of a cable model with an artificial rivulet is first carried out to obtain the aerodynamic force coefficients of the cable model.

首先在风洞中对带人工水线的拉索模型进行了试验，得到了气动力随水线平衡角的变化关系。

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Aerodynamic design characteristic of test cell for-high. by-pass ratio turbofan engine

大函道比涡扇发动机试车台气动力设计的特点

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By extending length of the test floor properly, the aerodynamic drag coefficient can be measured more precisely.

适当延长地板，可提高气动阻力系数的测量精度。

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The results show that the wind barrier on the bridge can decrease the train aerodynamic forces obviously, and the wind tunnel test match well with parts of numerical results.

试验表明：桥上设置风障可以明显减小列车的气动力，列车气动力结果与部分数值结果吻合较好。

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In this paper, the subsonic unsteady aerodynamic performance of a noncoplanar wing-tail combination can be computed on condition that the velocity potential function of unsteady vortex ring is taken as an elementary solution and the method of time history ( MTH) is used.

本文以非定常涡环速度势函数为基本解，应用时间历程方法，计算非共面机一尾翼组合体的非定常气动力性能。

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Influence of stator shroud on aerodynamic performance of axial-flow compressor and thermodynamic test results of a 4500 HP locomotive gas turbine

静叶内围带对轴流式压气机气动性能的影响及4500马力机车燃气轮机的热力性能

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Aerodynamic Design Method of Cascade Profiles Based on Load and Blade Thickness Distribution

基于气动载荷与叶片厚度分布的叶栅气动设计方法

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By modifying the thickness of the blade trailing edge, research influences of the blade trailing edge to the aerodynamic performance and noise levels.

通过修改叶型尾缘厚度，研究叶型尾缘厚度对风洞风扇的气动性能和噪声水平的影响。

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For example, an aerodynamic model might be incompressible thin airfoil theory;

例如，一个空气动力学模型可以是不可压的薄翼理论；

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The content of this paper includes the momentum& blade element theory and CFD method which are both used to compute the aerodynamic characteristics of cooling fans.

本文分别利用结合动量&叶素理论的经典计算方法和CFD方法计算不同型号的汽车冷却风扇的流场和气动特性，并进行比较。

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Starting with the dynamic analysis and the aerodynamic characteristics of the wing structure, the thin wing theory is introduced to analyze the stresses exerted on the cuttings, and then the minimum gas rate for effective cuttings removal during high-angle horizontal well gas drilling is discussed.

从力学分析入手，根据空气动力学翼型的气动特性，引入薄翼理论，对岩屑颗粒进行受力分析，探讨了气体钻大斜度水平井有效携带岩屑的最小排量问题。

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The calculation method for subsonic longitudinal and lateral aerodynamic characteristics of complete aircraft configuration

亚声速全机纵横向气动特性计算方法

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Multidisciplinary Aerodynamic/ Structural Design Optimization for High Subsonic Transport Wing Using Approximation Technique

基于近似技术的高亚声速运输机机翼气动/结构优化设计

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To obtain good aerodynamic characteristics, the radial aerodynamic balance equations were adopted to build the fan's rotating blades, which were evolved from the simplified three dimensional flow theories, the constraint conditions and the control vortex theory.

采用简化的三元流动设计理论得到叶轮叶片气动设计径向平衡方程式和求解约束条件，进而引入了控制涡设计理论进行风扇叶片造型，获得了优良的气动性能；

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In Chapter 3, the parameterization method and aerodynamic optimization method based on configuration dynamic evolution control for two-dimensional airfoil shape and three-dimensional lifting body are introduced.

第三章介绍了本文的二维翼型与三维升力体外形的参数化方法和基于外形动态演化控制的气动优化方法。

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Based on aerodynamic theory, the article elucidates the characteristics of the shockwave around a supersonic projectile and its utilization& principles of projectile target deviation measurement.

本文根据空气动力学理论，阐述了超音速弹丸的激波特性和利用该特性来测量弹目偏差的原理。

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