Progress in high-lift aerodynamic calculations
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46642
Reference30 articles.
1. Numerical analysis of multiple element high lift devices by Navier Stokes equation using implicit TVD finite volume method
2. Navier-Stokes solution for high-lift multielement airfoil system with flap separation
3. A comparative study of turbulence models for overset grids
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