Data-Based Approach for Fast Airfoil Analysis and Optimization
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057129
Reference38 articles.
1. XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils
2. Geometric Comparison of Aerofoil Shape Parameterization Methods
3. Universal Parametric Geometry Representation Method
4. Wing Design by Numerical Optimization
5. Aerofoil Design Variable Extraction for Aerodynamic Optimization
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