Summary of code validation results for a multiple element airfoil test case
Author:
Affiliation:
1. de Havilland, Inc., Bombardier Aerospace Group, Downsview, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1932
Reference20 articles.
1. Viscous-inviscid analysis of transonic and low Reynolds number airfoils
2. Progress in high-lift aerodynamic calculations
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