Use of Reduced, Accurate Ethylene Combustion Mechanisms for a Hydrocarbon-Fueled Scramjet Simulation
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American Institute of Aeronautics and Astronautics
Reference3 articles.
1. Hydrogen/air combustion calculations - The chemical basis of efficiency in hypersonic flows
2. A comprehensive modeling study of iso-octane oxidation
3. Hitch, B.D. "Reduced, Accurate Combustion Mechanisms for Reacting Flow CFD," paper no. AIAA-2009-5496presented at the45thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, CO, Aug.2-5 (2009).
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