亚音速飞行性能
Effects of free-stream turbulence on performance of subsonic diffuser
自由流紊流度对亚音速扩压器性能的影响
Effect of Inlet Velocity Distribution on the Flow and Performance of Subsonic Two-Dimensional Diffuser
进口速度分布对二元亚音速扩压器的流动和性能的影响
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。
Design and calculation of performance of a subsonic inlet duct
亚音速飞行器进气道内通道设计及性能计算
Design and Performance of S-shaped Inlet for High Subsonic Missiles
一种高亚音速弹用S弯进气道设计及其特性
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