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The paper focuses on the turbo ramjet engine, which is a kind of airbreathing engine.It is expected to apply for hypersonic transport propulsion system. In the process fromturbo mode to ramjet mode, the turbo ramjet composed engine operates through the way ofcombined cycle. In this paper the combined cycle performance was simulated for two layouts.The results show that the laws are feasible.
The paper focuses on the turbo ramjet engine, which is a kind of airbreathing engine. It is expected to apply for hypersonic transport propulsion system. In the process from turbo mode to ramjet mode, the turbo ramjet composed engine operates through the way ofcombined cycle. In this paper the combined cycle performance was simulated for two layouts. The results show that the laws are feasible.