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Numerical study on the flow characteristics and stability in the isolator of rotating detonation ramjet engine by different combustion modes and structure parameters

Numerical StudyAeroacousticsEngineeringDetonation PhenomenonAerospace EngineeringStructure ParametersGas Turbine CombustionIn-cylinder FlowAerodynamicsDetonation Ramjet EnginePropulsionFuel InjectionSupersonic Combustion