Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method
Author:
Affiliation:
1. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2237
Reference14 articles.
1. Two-point transonic airfoil design using optimization for improved off-design performance
2. Genetic Algorithms + Data Structures = Evolution Programs
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