This paper introduces some results of theoretical and experimental aerodynamicinvestigation of base bleed by solid fuel combustion.
本文介绍固体燃料底部排气燃烧空气动力理论及实验研究的若干结果。
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For investigating the aerodynamic character of the turbine cascades, understanding the detail flow in turbine cascades, the computational investigation was applied on some type turbine guide vane.
The range equipment for the investigation of the hypervelocity aerodynamic properties and flow field of explosively formed projectile(EFP) models is described.