Dynamic boundary control system for detonation dynamic stable propagation in supersonic airflow
A technology of dynamic stability and boundary control, applied in ramjet engines, machines/engines, jet propulsion devices, etc., can solve the problem that the conceptual design of the new scramjet engine has not been reported, and achieve the effect of flexible and efficient control functions
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[0022] In order to make the technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0023] The embodiment of the present invention proposes a dynamic boundary control system for the dynamic and stable propagation of detonation in supersonic airflow, figure 1 is a schematic diagram of the structure of this embodiment, such as figure 1 As shown, it includes a detonation wave state monitoring system, an information analysis module, and an expansion wall adjustment control system. The expansion wall adjustment control system includes an expansion wall and an expansion wall power system, and at least one expansion wall 3 capable of adjusting the expansion angle of the wall of the combustion ...
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