Pressurization flow control device-containing SERN structure for TBCC
A technology of flow control and supercharger, applied in the directions of jet propulsion, machine/engine, climate sustainability, etc., can solve the problems of increasing engine weight, increasing radar reflection area, increasing design cost, etc., to improve over-expansion The working conditions, the reduction of the separation area, and the effect of improving the quality of the flow field
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[0013] The above and other technical features and advantages of the present invention will be described in more detail below in conjunction with the accompanying drawings.
[0014] see figure 1 As shown, it is the SERN structure of the TBCC with pressurized flow control device of the present invention and the overall composition of the high-speed aircraft, which includes the lower wall surface 4 of the single-slope expansion nozzle, the contraction section 6 of the single-slope expansion nozzle and the single-slope expansion nozzle. The unilateral expansion section 5 of the nozzle; it also includes a pressurized flow device arranged on the unilateral expansion section 5 of the single-slope expansion nozzle.
[0015] The pressurized flow device in this embodiment includes a U-shaped communication pipeline 7 and a supercharger 8 arranged on the U-shaped communication pipeline 7, and the front port of the U-shaped communication pipeline 7 is placed in an oblique shock wave and si...
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