Validation of Computations Around High-Lift Configurations by Structured- and Unstructured-Mesh
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
2. Ryoyu Systems Company, Ltd., Tokyo 108-0074, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15445
Reference29 articles.
1. Multi-Element High-Lift Configuration Design Optimization Using Viscous Continuous Adjoint Method
2. Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing
3. Efficient Optimization Design Method Using Kriging Model
4. Prediction of high lift: review of present CFD capability
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