Multiobjective Aerodynamic Optimization by Variable-Fidelity Models and Response Surface Surrogates
Author:
Affiliation:
1. Iowa State University, Ames, Iowa 50011
2. Gdańsk University of Technology, 80-233 Gdańsk, Poland
3. Reykjavik University, 101 Reykjavik, Iceland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054128
Reference38 articles.
1. Numerical Optimization for Advanced Turbomachinery Design
2. Derivatives for Time-Spectral Computational Fluid Dynamics Using an Automatic Differentiation Adjoint
3. Heat Transfer Optimization of Gas Turbine Blades Using an Adjoint Approach
4. Aerodynamic Shape Optimization of Wings Using a Parallel Newton-Krylov Approach
5. Constrained Aerodynamic Optimization of Three-Dimensional Wings Driven by Navier-Stokes Computations
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