Performance Analysis of a Hybrid Pulse Detonation Combustor/Gas Turbine System
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Publisher
American Institute of Aeronautics and Astronautics
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1. Experimental investigation on interactions between a two-phase multi-tube pulse detonation combustor and a centrifugal compressor;Applied Thermal Engineering;2017-02
2. Foundational Performance Analyses of Pressure Gain Combustion Thermodynamic Benefits for Gas Turbines;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
3. Time-Accurate Flow Field and Rotor Speed Measurements of a Pulsed Detonation Driven Turbine;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
4. A Simplified Model for Detonation Based Pressure-Gain Combustors;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25
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