High-Lift Wing Design in Consideration of Sweep Angle Effect Using Kriging Model
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
2. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-175
Reference16 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. High-Lift Aerodynamics
3. Multi-Objective Aerodynamic Exploration of Elements' Setting for High-Lift Airfoil Using Kriging Model
4. High-lift design optimization using Navier-Stokes equations
5. Pepper. R. S., van Dam C. P., and Gelhausen P. A. "Design Methodology for High-lift System on Subsonic Transport Aircraft," AIAA-96-4056-CP,4056
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