Comparison of flux-vector and flux-difference splitting techniques for hypersonic flow
Author:
Affiliation:
1. Lockheed Engineering and Management Services Co., Inc., Houston, TX
2. NASA, Johnson Space Center, Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-3647
Reference6 articles.
1. R. P. Reklis, and P. D. Thomas, Shock-Capturing Algorithm for the Navier-Stokes Equations, AIAA-81-1021 (1981)
2. J. Y. Yang, Numerical Solutzon of the Two-Dimensional Euler Equattons by Second-Order Upwind Difference Schemes, AIAA-85-0292 (1985)
3. S. X. Ying, Numerical Simulation of tinsteady, Viscous, High-Angle-of-Attack flouis Using A Partially Flux-Split Algortthm, AIAA-86-2179 (1986)
4. The use of the Riemann problem in finite difference schemes
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