Evaluation of Computations and Transition Prediction Method for Aircraft High-Lift Configuration
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
2. Tokyo Business Service Company, Ltd., Tokyo 160-0023, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34948
Reference41 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. Prediction of high lift: review of present CFD capability
3. Experimental investigation of a simplified 3D high lift configuration in support of CFD validation
4. CFD validation of high-lift flows with significant wind-tunnel effects
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2. Influence of Transition on High-Lift Prediction with the NASA Trap Wing Model;29th AIAA Applied Aerodynamics Conference;2011-06-27
3. Improving the Prediction for the NASA High-Lift Trap Wing Model;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
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