Application of the implicit MacCormack scheme to the parabolized Navier-Stokes equations
Author:
Affiliation:
1. Iowa State University, Ames, Iowa
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8848
Reference19 articles.
1. Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
2. 2Schiff, L. B. and Steger, J. L. "Numerical Simulation of Steady Supersonic Viscous Flow," AIAA Paper 79-0130, Jan.1979.
3. Alternating direction implicit techniques for two-dimensional magnetohydrodynamic calculations
4. Three-dimensional supersonic flow of a viscous or inviscid gas
5. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
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