Numerical investigation of operational performance in a methane-oxygen rotating detonation rocket engine
Author:
Affiliation:
1. Sierra Lobo, Inc.
2. University of California, Los Angeles
3. HyPerComp, Inc.
4. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference23 articles.
1. Feasibility studies of a rotating detonation wave rocket motor.
2. Thermodynamic Cycle Analysis of Pulse Detonation Engines
3. Idealized Efficiency Calculations for Rotating Detonation Engine Rocket Applications
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