Development of a flexible and efficient multigrid-based multiblock flow solver
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Analytical Services and Materials, Inc., Hampton, VA
3. Vigyan, Inc., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-677
Reference27 articles.
1. Jameson, A, Baker, T.J.; and Weatherill. N.P. "Calculation of Inviscid Transonic Flow Over a CompleteAircraft". AIAAPaper 864103,January, 1986.
2. Development of a multigrid code for 3-D Navier-Stokes equations and its application to a grid-refinement study
3. Radespiel,R. "A Cell-VertexMultigrid Method for the Navier-Stokes Equations". NASA TM 101557, January 1989.
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