Efficient Aerodynamic Design using the Discrete Adjoint Method in SU2-Reference-Cited by-同舟云学术

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Efficient Aerodynamic Design using the Discrete Adjoint Method in SU2

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
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Author:

Albring Tim A.¹,Sagebaum Max¹,Gauger Nicolas R.¹

Affiliation:

1. Technical University of Kaiserslautern

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3518

Reference38 articles.

1. Aerodynamic design via control theory

2. Control theory based airfoil design using the Euler equations

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