Implicit upwind residual-distribution Euler and Navier-Stokes solver on unstructured meshes
Author:
Affiliation:
1. von Karman Institute for Fluid Dynamics, Rhode-St-Genese B-1640, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13348
Reference31 articles.
1. Solution of the Euler equations for two dimensional transonic flow by a multigrid method
2. Solution of the three-dimensional compressible Navier-Stokes equations by an implicit technique
3. Discretized Newton-relaxation solution of high resolution flux-difference split schemes
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