RDE Nozzle Computational Design Methodology Development and Application
Author:
Affiliation:
1. NASA Glenn Research Center
2. Ohio Aerospace Institute
Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
1. Experimental and Numerical Evaluation of Pressure Gain Combustion in a Rotating Detonation Engine
2. Comparison of Numerically Simulated and Experimentally Measured Performance of a Rotating Detonation Engin
3. Impact of an Exhaust Throat on Semi-Idealized Rotating Detonation Engine Performance
4. Comparison of Numerically Simulated and Experimentally Measured Performance of a Rotating Detonation Engin
5. Operational Stability Limits in Rotating Detonation Engine Numerical Simulations
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1. Flow Development in Radial Plane of Rotating Detonation Engine Integrated with Aerospike;Journal of Propulsion and Power;2023-05
2. Variably Premixed Rotating Detonation Engine for Evaluation of Detonation Cycle Dynamics;Journal of Propulsion and Power;2023-05
3. Flow acceleration in an RDRE with gradual chamber constriction;Shock Waves;2023-02-06
4. Nozzle Design for Rotating Detonation Engine;Journal of Propulsion and Power;2022-09
5. Computational Fluid Dynamic Optimization of an Experimental Rotating Detonation Rocket Engine Nozzle;AIAA AVIATION 2022 Forum;2022-06-20
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