Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet
Author:
Affiliation:
1. University of Queensland, Brisbane, Queensland 4072, Australia
Funder
Australian Government Research Training Program Scholarship
Australian Research Council Discovery Project funding scheme
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057417
Reference28 articles.
1. Supersonic combustion of hydrocarbons in a shape-transitioning hypersonic engine
2. Effects of Oxygen Enrichment on Scramjet Performance
3. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11
4. Tailored Fuel Injection for Performance Enhancement in a Mach 12 Scramjet Engine
5. Experimental Investigation of a Three-Dimensional Scramjet Engine at Mach 12
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