Output error method is one of the most widely applied methods in the region of aerodynamic parameter identification for aircraft.
输出误差法是飞行器气动参数辨识最广泛采用的一种方法。
Experiment and engineering approach have been applied to research aerodynamic characteristics of rarefied transitional flow around sphere-bicone configuration.
采用风洞试验和工程计算相结合的方法,对球双锥类外形的稀薄过渡流区气动特性进行了研究。
In order to adapt to new modern car styling, the aerodynamic numerical simulations based on computational fluid dynamics (CFD) are applied to the process of car styling.
结合作者进行的汽车造型概念设计,介绍了应用虚拟风洞进行汽车空气动力学数值模拟的研究过程。
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