A supersonic flow mixing device based on the jet disturbance at the trailing edge of the dividing plate
A technology of supersonic flow and mixing device, applied in rocket engine devices, jet propulsion devices, machines/engines, etc., can solve problems such as unsatisfactory effects, and achieve the effects of simple structure, high-efficiency mixing, and controllable jet flow
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[0017] In order to make the objectives, technical solutions and advantages of the present application more clear, the present application will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application, but not to limit the present application.
[0018] The supersonic flow mixing device based on the jet disturbance at the trailing edge of the separator plate provided in this application can be applied to the mixing chamber of the ejection mode of the rocket-based combined cycle engine. Among them, the first supersonic airflow is the compressed supersonic incoming air entering from the intake port, and the second supersonic airflow is the supersonic rich combustion gas accelerated by the expansion of the rocket combustion chamber through the tail nozzle, and the gas flowing out of the rocket combustion chamber is supersoni...
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