Evaluation of Euler solvers for transonic wing-fuselage geometries
Author:
Affiliation:
1. McDonnell Aircraft Company, St. Louis, Missouri 63166
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46113
Reference14 articles.
1. Transonic wing-body calculations using Euler equations
2. A new multigrid Euler method for fighter-type configurations
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