Airfoil Optimization Using Practical Aerodynamic Design Requirements
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000256
Reference19 articles.
1. Transonic Airfoil Shape Optimization in Preliminary Design Environment
2. Comparative Study of Three-Dimensional Wing Drag Minimization by Different Optimization Techniques
3. Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil Transport
4. Aerodynamic Optimization Under a Range of Operating Conditions
5. Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
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