In this paper, the subsonic unsteady aerodynamic performance of a noncoplanar wing-tail combination can be computed on condition that the velocity potential function of unsteady vortex ring is taken as an elementary solution and the method of time history ( MTH) is used.
本文以非定常涡环速度势函数为基本解,应用时间历程方法,计算非共面机一尾翼组合体的非定常气动力性能。
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