Navier-Stokes simulations of transonic flows over a wing-fuselage combination
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo, Japan
2. University of Tokyo, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9829
Reference16 articles.
1. Hoist, T.L., etal, AIAA Paper 85-1640, July 1985.
2. A NEW PREDICTOR-CORRECTOR SCHEME FOR THE SIMULATION OF THREE-DIMENSIONAL COMPRESSIBLE FLOWS WITH SEPARATION
3. Simulation of wing, fuselage, and wing/fuselage flowfields using a three-dimensional Euler/Navier-Stokes algorithm
4. An approximate LU factorization method for the compressible Navier-Stokes equations
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