Development of a Hybrid Unstructured Implicit Solver for the Simulation of Reacting Flows Over Complex Geometries
Author:
Affiliation:
1. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2227
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4. Effect of Vibrational Nonequilibrium on Hypersonic Double-Cone Experiments
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