An implicit flux-difference splitting scheme for three-dimensional, incompressible Navier-Stokes solutions to leading edge vortex flows
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Kansas, University, Lawrence
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1839
Reference28 articles.
1. Euler EquationsI" ICASE- Report No. 82-30, Sept. 1982. '[4] Moretti, G. "An Old Integration Scheme for
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