Single/two-objective aerodynamic shape optimization by a Stackelberg/adjoint method-Reference-Cited by-同舟云学术

Single/two-objective aerodynamic shape optimization by a Stackelberg/adjoint method

Published:2019-06-26 Issue:5 Volume:52 Page:753-776
ISSN:0305-215X
Container-title:Engineering Optimization
language:en
Short-container-title:Engineering Optimization

Author:

Wang Jing¹,Zheng Yao¹,Chen Jianjun¹,Xie Fangfang¹,Zhang Jifa¹,Périaux Jaques²,Tang Zhili³

Affiliation:

1. Center for Engineering and Scientific Computation, and School of Aeronautics and Astronautics, Zhejiang University, Zhejiang, PR China

2. International Center for Numerical Methods in Engineering (CIMNE), Barcelona, Spain

3. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, PR China

Funder

Zhejiang Provincial Natural Science Foundation

Science Challenge Project of China

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Link

https://www.tandfonline.com/doi/pdf/10.1080/0305215X.2019.1618287

Reference19 articles.

1. A NOTE ON WEIGHTED CRITERIA METHODS FOR COMPROMISE SOLUTIONS IN MULTI-OBJECTIVE OPTIMIZATION

2. Game Theory with Engineering Applications

3. Continuous Adjoint Approach for the Spalart-Allmaras Model in Aerodynamic Optimization

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