本文介绍一种带操纵面机翼的非定常跨声速流的有限差分计算方法。
A numerical method is presented for predicting unsteady transonic aerodynamic flow about aircraft wings with control surface.
本论文采用直接表面曲率迭代方法(DISC)进行跨声速翼型设计。
In this paper the Direct Iterative Surface Curvature (DISC) design method is presented for designing airfoils at transonic speeds.
本文介绍一种设计跨声速自然层流翼型的计算流体力学（CFD）方法。
This paper represents a CFD method for the design of NLF airfoils directly under transonic viscous flow conditions.
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