Combustion Stabilization in an Axisymmetric Scramjet in Mach 4.5 Flows
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1681
Reference21 articles.
1. Hypersonic Airbreathing Propulsion
2. The Scramjet Engine
3. Visualizing supersonic inlet duct unstart using planar laser Rayleigh scattering
4. Ethylene Flame Dynamics and Inlet Unstart in a Model Scramjet
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3. Numerical Investigation of an Axisymmetric Model Scramjet Assisted with Cavity of Different Aft Wall Angles;International Journal of Aerospace Engineering;2021-08-02
4. Ethylene Combustion in an Axisymmetric Mach 4.5 Cavity;AIAA Scitech 2021 Forum;2021-01-04
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