Calculation of Supersonic Combustion Using Implicit Schemes
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3181
Reference7 articles.
1. Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations
2. Numerical study of chemically reacting flows using a lower-upper symmetric successive overrelaxation scheme
3. Fully coupled implicit method for thermochemical nonequilibrium air at suborbital flight speeds
4. Three-dimensional calculations of supersonic reacting flows using an LU scheme
5. Effect of artificial diffusion schemes on multigrid convergence
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1. Computational Challenges in Hypersonic Flow Simulations;39th AIAA Thermophysics Conference;2007-06-15
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