Measurements for Fuel Reforming for Scramjet Thermal Management and Combustion Optimization: Status of the COMPARER Project
Author:
Affiliation:
1. Orleans University
2. MBDA France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8005
Reference15 articles.
1. French Hypersonic Propulsion Program PREPHA - Results, lessons and perspectives
2. Bouchez, M., and Beyer, S. "PTAH-SOCAR fuel cooled composite material structure for dual mode ramjet and liquid rocket engine - 2005 status", AIAA2005-3434.
3. Serre, L., Falempin, F. "PROMETHEE : The French military hypersonic propulsion Program", AIAA-2002-5141.
4. Experimental and Numerical Investigations of an Endothermic Fuel Cooling Capacity for Scramjet Application
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