Aerodynamic forces; 2D morphing - numerical simulations - incidence 1.8 deg - static case
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资源简介：
ASCII file containing aerodynamic forces around an A320 wing. From a 2D numerical simulation performed with the NSMB code. The first four columns give the physical time in seconds, the drag coefficient, the lift coefficient and the pitching moment coefficient for a morphing wing. The trailing edge not vibrating, it is the so-called static case.
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Root创建时间：
2021-04-02
