Massively Multipoint Aerodynamic Shape Design via Surrogate-Assisted Gradient-Based Optimization
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Funder
111 Project of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference61 articles.
1. State-of-the-art in aerodynamic shape optimisation methods
2. Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing
3. Surrogate-based aerodynamic shape optimization with the active subspace method
4. Aerodynamic design via control theory
5. A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization
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