Validation of Transient Cooling Modeling for Hypersonic Application
Author:
Affiliation:
1. Université d’Orléans, 18000 Bourges, France
2. MBDA-France, 18000 Bourges, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.26022
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1. A Century of Ramjet Propulsion Technology Evolution
2. Scramjet Engines: The First Forty Years
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