FIRE II Calculations for Hypersonic Nonequilibrium Aerothermodynamics Code Verification: DPLR, LAURA, and US3D
Author:
Affiliation:
1. NASA Ames Research Center
2. ELORET Corporation
3. NASA Langley Research Center
4. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-605
Reference55 articles.
1. Data-Parallel Line Relaxation Method for the Navier-Stokes Equations
2. Aerothermal Analysis of the Project Fire II Afterbody Flow
3. 4Gnoffo, P. A. "An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous, Compressible Perfect-Gas Flows," NASA TP-2953,1990.
4. 5Nompelis, I., Drayna, T. W., and Candler, G. V. "A Parallel Unstructured Implicit Solver for Hypersonic Reacting Flow Simulation,"AIAA Paper 2005-4867,2005.
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