Navier-Stokes simulation of transonic flow over wing-fuselage combinations
Author:
Affiliation:
1. National Aerospace Laboratory, Chofu, Japan
2. Tokyo, University, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1831
Reference14 articles.
1. Numerical solution of transonic wing flows using an Euler/Navier-Stokes zonal approach
2. LU factorization of an implicit scheme for the compressible Navier-Stokes equations
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