An unstructured grid parallel MHD solver for real gas simulations
Author:
Affiliation:
1. HyPerComp, Inc., Westlake Village, CA
2. Boeing-Rocketdyne Propulsion and Power, Canoga Park, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2738
Reference20 articles.
1. An upwind differencing scheme for the equations of ideal magnetohydrodynamics
2. Felderman, E.J., and MacDermott, W.N. "Near-Electrode Model with Nonequilibrium lonization (at 100 atm,)AIAA 95-1993, June 1995 Hoffmann, K.A., Damevin, H.M., Dietiker, J.F. "Numerical simulation of hypersonic magnetohydrodynamic flows," AIAA 2000-2259
3. Nonequilibrium ionization due to electron heating - i - theory
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1. Effect of Wall Conduction in Proposed MHD Enhanced Hypersonic Vehicles;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15
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