Calculate the lift and drag over simple aerodynamic shapes in compressible, inviscid flows.
能估算可压缩无粘流中，基本空气动力外形的升力和阻力。
A numerical method for calculating steady inviscid transonic flows over wings is introduced in this paper.
本文介绍机翼无粘定常跨音速绕流的一种数值计算方法。
A numerical method for calculating steady inviscid transonic flows over wings is introduced in this paper.
本文介绍机翼无粘定常跨音速绕流的一种数值计算方法。
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