Transitional Flow Modeling and Application to High-Lift Multi-Element Airfoil Configurations
Author:
Affiliation:
1. Deutsche Forschungsanstalt fur¨ Luft- und Raumfahrt, German Aerospace Center, D-38108 Brunswick, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3159
Reference22 articles.
1. Transition predictions using Reynolds-averaged Navier-Stokes and linear stability analysis methods
2. Feasibility Study of e Transition Prediction in Navier-Stokes Methods for Airfoils
3. Computation of compressible, laminar boundary layers on swept, tapered wings
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