Computational Modeling Advances Supporting Hypersonic Scramjet Design
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8037
Reference17 articles.
1. Studies of scramjet performance in the LENS facilities
2. A Parallel Adaptation Package For Three-Dimensional Mixed-Element Unstructured Meshes
3. Transpiration Cooling Performance in LOX/Methane Liquid-Fuel Rocket Engines
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