Aerodynamic Design of Transonic Wings Using the Target Pressure Optimization Approach
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/10.2514/2.2374
Reference15 articles.
1. Genetic optimization of target pressure distributions for inverse design methods
2. Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method
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