Design Optimization of Subsonic Airfoil and Slotted Flap Shape Using Multi-Fidelity Aerodynamic Analysis
Author:
Affiliation:
1. Konkuk University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2704
Reference16 articles.
1. A Universal Parametric Geometry Representation Method - "CST"
2. 3W.H.Wentz, “Wind tunnel tests of the GA W-2 airfoil with 20% aileron, 25% slotted flap, 30% fowler flap and 10% slot-lip spoiler,” Tech. Rep. NASA CR-145139, 1976.
3. Subsonic Airfoil and Flap Hybrid Optimization Using Multi-Fidelity Aerodynamic Analysis
4. Multi-Element High-Lift Configuration Design Optimization Using Viscous Continuous Adjoint Method
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