Publication | Open Access
Combining LES of combustion chamber and an actuator disk theory to predict combustion noise in a helicopter engine
43
Citations
42
References
2016
Year
AeroacousticsEngineeringNoise ControlAerospace EngineeringMechanical SystemsNoiseSystems EngineeringRotor DynamicIn-cylinder FlowPropulsionHelicopter EngineActuator Disk TheoryCombustion Chamber
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