Numerical Investigation on Combustion-Enhancement Strategy in Shock–Fuel Jet Interaction
Author:
Affiliation:
1. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060168
Reference76 articles.
1. Fluid Phenomena in Scramjet Combustion Systems
2. Behaviour of small regions of different gases carried in accelerated gas flows
3. Vorticity generation by shock propagation through bubbles in a gas
4. Progress toward shock enhancement of supersonic combustion processes
5. MarbleF. E.ZukoskiE. E.JacobsJ.HendricksG.WaitzI. “Shock Enhancement and Control of Hypersonic Mixing and Combustion,” Vol. 31, AIAA, Washington, D.C., 1990, pp. 854–862. 10.2514/6.1990-1981
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