Compressible Navier-Stokes computations of multielement airfoil flows using multiblock grids
Author:
Affiliation:
1. University of Toronto, Downsview, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12014
Reference20 articles.
1. Developments in computational methods for high-lift aerodynamics
2. Calculation of flow over multielement airfoils at high lift
3. Efficient simulation of incompressible viscous flow over single and multi-element airfoils
4. Navier-Stokes solution for high-lift multielement airfoil system with flap separation
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1. Effect of Flap and Slat Riggings on 2-D High-Lift Aerodynamics;Journal of Aircraft;2006-09
2. Low Frequency Oscillations Of Thin Airfoils In Subsonic Compressible Flows;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
3. Efficient second-order analytical solutions for airfoils in subsonic flows;Aerospace Science and Technology;2005-03
4. Multipoint and Multi-Objective Aerodynamic Shape Optimization;AIAA Journal;2004-06
5. Optimization of High-Lift Configurations Using a Newton-Krylov Algorithm;16th AIAA Computational Fluid Dynamics Conference;2003-06-23
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