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Ramjet Engine with Rotating Detonation Combustion System and Method for Operation
Ramjet Engine with Rotating Detonation Combustion System and Method for Operation
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机译:带有旋转爆震燃烧系统的Ramjet发动机及其运行方法
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摘要
A ramjet engine and system and method for operation is generally provided. The ramjet includes a longitudinal wall extended along a lengthwise direction. The longitudinal wall defines an inlet section, a combustion section, and an exhaust section. A fuel nozzle assembly is extended from the longitudinal wall. The fuel nozzle assembly defines a nozzle throat area. The fuel nozzle assembly is moveable along a radial direction to adjust the nozzle throat area based at least on a difference in pressure of a flow of fluid at an inlet of the inlet section and a pressure of the flow of fluid at the fuel nozzle assembly.
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