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对一个带有双发动机的战术导弹通气模型在测力、测压内外流气动特性上的测量结果表明:导弹进气口通气与不通气加堵锥状态对全弹气动特性的影响不容忽视,进而说明导弹通气模型实验是十分必要的。
The measurement results on the aerodynamic characteristics of a dual-engine tactical missile ventilation model in terms of force and pressure inside and outside the flow show that the influence of the missile inlet ventilation and the non-ventilation and the plugging cone on the overall aerodynamic characteristics can not be ignored, and thus It is very necessary to explain the experiment of missile ventilation model.