Suppression of Premature Ignition in the Pre-mixed Inlet Flow of a Shcramjet
Author:
Affiliation:
1. University of Toronto
2. Seoul National University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5187
Reference22 articles.
1. Numerical Simulation of Hypersonic Shock-Induced Combustion Ramjets
2. Historical Survey on Enhanced Mixing in Scramjet Engines
3. Penetration and Spreading of Liquid Jets in an External-Internal Compression Inlet
4. Effects of Fuel Preinjection on Mixing in Mach 1.6 Airflow
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Mitigation of Autoignition Due to Premixing in a Hypervelocity Flow Using Active Wall Cooling;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12
2. Study of Forebody Injection and Mixing with Application to Hypervelocity Airbreathing Propulsion;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
3. Research status of key techniques for shock-induced combustion ramjet (shcramjet) engine;Science in China Series E: Technological Sciences;2010-01
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