aerodynamic analysis and test 气动分析和试验
aerodynamic characteristic analysis 气动特性分析
aerodynamic characteristics analysis 气动特性分析
aerodynamic performance comprehensive analysis 气动性能综合分析
time-of-flight aerodynamic particle size analysis 飞行时间空气动力学气雾粒径测定法
An aerodynamic model is developed based on unsteady aerodynamic mechanisms for the purpose of aerodynamic analysis of a flapping-wing micro air vehicle.
初步探讨了翅翼产生升力的非定常气动力特征，提出了微扑翼飞行器的机翼气动模型，在进行了翼型设计的基础上，对翅翼机构进行了气动分析，研究了翅翼拍频、风速对气动力的影响。
参考来源 - 基于数学形态学的微扑翼飞行器翅翼机构设计·2,447,543篇论文数据，部分数据来源于NoteExpress
Panel Method was used for subsonic aerodynamic analysis, and the Modified Newtonian Impact Theory was used for hypersonic aerodynamic analysis.
亚声速气动力采用面源法计算，高超声速气动力采用修正的牛顿流理论计算。
For subsonic aerodynamic analysis, Linearized Velocity Potential Theory is used to evaluate the aerodynamic coefficient, and we can get subsonic aerodynamic model of vehicle by Regression analysis.
在进行亚音速气动分析时，应用线化速度势理论计算运载器的气动力系数，而后进行回归分析，得到运载器亚音速飞行时的气动特性模型。
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