Aerodynamic Redesign Using Discrete Adjoint Approach on Overset Mesh System
Author:
Affiliation:
1. Seoul National University, Seoul 151-744, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34112
Reference25 articles.
1. Aerodynamic design via control theory
2. Airfoil Shape Optimization Using Sensitivity Analysis on Viscous Flow Equations
3. Aerodynamic Shape Optimization of Wings Including Planform Variations
4. Two-Level Multi-Fidelity Design Optimization Studies for Supersonic Jets
5. Automated design methodology of turbulent internal flow using discrete adjoint formulation
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