Numerical Analysis of a Scramjet Engine with Intake Sidewalls and Cavity Flameholder
Author:
Affiliation:
1. School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang Gyeonggi-do 412-791, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051677
Reference26 articles.
1. Flame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity Flameholder
2. Mixing and Combustion Characteristics of Kerosene in a Model Supersonic Combustor
3. Investigation of Kerosene Combustion Characteristics with Pilot Hydrogen in Model Supersonic Combustors
4. CFD Analysis of the HyShot II Scramjet Experiments in the HEG Shock Tunnel
5. Three-dimensional numerical study of a scramjet combustor
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