Modeling Swirl Evolution Inside Annular Nozzles Under Compressible Effect
Author:
Affiliation:
1. Sogang University, Seoul 04107, Republic of Korea
2. Seoul National University, Seoul 08826, Republic of Korea
3. Korea Institute of Energy Research, Daejeon 34129, Republic of Korea
Funder
Korea Institute of Energy Research
National Research Foundation of Korea
Korea Electric Power Research Institute
Samsung Electronics Co., Ltd.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061532
Reference46 articles.
1. Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight
2. Vortex mixing for supersonic combustion
3. SettlesG. S. “Supersonic Mixing Enhancement by Vorticity for High-Speed Propulsion,” NASA CR 188920, 1991.
4. Near-field flow of supersonic swirling jets
5. Vortex Flow in a Convergent-Divergent Nozzle
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