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The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A 15% increase in thermal efficiency at medium pressure ratios is promised by rotating detonation engine technology over conventional Joule–Bryton cycles. A supersonic inlet turbine is a viable option to extract substantial ...
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A supersonic inlet turbine can extract substantial energy from the highly fluctuating and transonic flow delivered by a rotating detonation combustor (RDC). However, a transition duct is necessary to achieve the supersonic ...
The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Rotating detonation engines (RDEs) are characterized by a thermodynamic cycle with an efficiency gain up to 15% at medium pressure ratios with respect to systems based on the conventional Joule–Bryton cycle. Multiple turbine ...