A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equations
Author:
Affiliation:
1. Rutgers University, New Brunswick, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8738
Reference46 articles.
1. *Law, C. H."Three-Dimensional Shock Wave-Turbulent Boundary Layer Interactions at Mach 6, "Aerospace Research Laboratories, Wright-Patterson AFB, Ohio, ARL-TR-75-0191, June 1975.
2. 3Oskam, B., Vas., I. E., and Bogdonoff, S. M. "Mach 3 Oblique Shock Wave/Turbulent Boundary Layer Interactions in Three Dimensions," AIAA Paper 76-336,1976.
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