Two-Step optimization based on CST-cGANs for airfoil inverse design
Author:
Affiliation:
1. Sun Yat-sen University, China
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3670105.3670112
Reference24 articles.
1. Gao Zhenghong and Wang Chao.2017.Research and progress on aerodynamic shape design methods of aircraft.Acta Aerodynamica Sinica,35,516-528.
2. S TAKANASHI.1985.Iterative three-dimensional transonic wing design using integral equations.Journal of Aircraft.
3. Kim S,Alonso J,and Jameson A.2002.Design optimization of high-lift configurations using a viscous continuous adjoint method.In 40th AIAA Aerospace Sciences Meeting amp;Exhibit.
4. Tan Bui-Thanh Murali Damodaran and Karen E Willcox.2004.Aerodynamic data reconstruction and inverse design using proper orthogonal decomposition.AIAA Journal.
5. LIU Ling-jun ZHOU Yue and GAO Zhen-xun.2018.Aerodynamic force calculation and inverse design for airfoil based on neural network. 3 5 41-47.
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