Rotating Detonation Engine Interaction with an Annular Ejector
Author:
Affiliation:
1. Innovative Scientific Solutions, Inc.
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0287
Reference7 articles.
1. A Simple Pressure-Gain Combustor for Gas Turbines
2. Ejector Enhanced Pulsejet Based Pressure Gain Combustors: An Old Idea With a New Twist
3. Valveless-Gas-Turbine Combustors With Pressure Gain
4. Performance of Choked Unsteady Ejector-Nozzles for use in Pressure Gain Combustors
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