Detonation Stabilization in Supersonic Flow: Effects of Suction Boundaries
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
2. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference30 articles.
1. Review of Propulsion Applications of Detonation Waves
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5. Numerical Analysis of a Scramjet Engine with Intake Sidewalls and Cavity Flameholder
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2. Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner;Journal of Fluid Mechanics;2022-04-11
3. Effects of velocity shear layer on detonation propagation in a supersonic expanding combustor;Physics of Fluids;2021-10
4. Eliminating Boundary Layer Separation on a Cylinder with Nonuniform Suction;International Journal of Aerospace Engineering;2020-07-22
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