Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50745
Reference34 articles.
1. A detached shock calculation by second-order finite differences
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3. Alternating direction implicit techniques for two-dimensional magnetohydrodynamic calculations
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