Profiling cross-sectional area of a radial rotating detonation combustor to increase pressure gain
Author:
Funder
Office of Naval Research
National Aeronautics and Space Administration
U.S. Department of Education
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference33 articles.
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2. High-fidelity simulations of pressure-gain combustion devices based on detonations;Kailasanath;J. Propuls. Power,2017
3. Rotating detonation combustors and their similarities to rocket instabilities;Anand;Prog. Energy Combust. Sci.,2019
4. Determining the pressure gain of pressure gain combustion;Kaemming,2018
5. Experimental study of the performance of a rotating detonation engine with nozzle;Fotia;J. Propuls. Power,2016
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