Robust Airfoil Optimization Using a Conditional Expected Maximum Value Approach
Author:
Affiliation:
1. Kennesaw State University, Kennesaw, Georgia 30144
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061565
Reference17 articles.
1. HuyseL.LewisR. M. “Aerodynamic Shape Optimization of Two-Dimensional Airfoils Under Uncertain Conditions,” ICASE NASA Langley Research Center TR 2001-1, Hampton, VA, 2001.
2. HuyseL. “Free-Form Airfoil Shape Optimization Under Uncertainty Using Maximum Expected Value and Second-Order Second-Moment Strategies,” ICASE NASA Langley Research Center TR 2001-18, Hampton, VA, 2001.
3. Probabilistic Approach to Free-Form Airfoil Shape Optimization Under Uncertainty
4. Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
5. LiW. “Profile Optimization Method for Robust Airfoil Shape Optimization in Viscous Flow,” NASA TM-2003-212408, 2003.
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