Multi-Objective Optimization of a Transonic Compressor Rotor by Using an Adjoint Method
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Peking University, 100871 Beijing, People’s Republic of China
2. Department of Mechanical and Aerospace Engineering, University of California, Irvine, California 92697-3975
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053436
Reference21 articles.
1. Three-Dimensional Multi-Objective Design Optimization of a Transonic Compressor Rotor
2. Multi-Objective Optimization of Transonic Compressor Blade Using Evolutionary Algorithm
3. Kriging Models for Global Approximation in Simulation-Based Multidisciplinary Design Optimization
4. Gappy Proper Orthogonal Decomposition-Based Two-Step Optimization for Airfoil Design
5. Aerodynamic design via control theory
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