Continuous Adjoint Approach for the Spalart-Allmaras Model in Aerodynamic Optimization-Reference-Cited by-同舟云学术

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

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Bueno-Orovio Alfonso¹,Castro Carlos¹,Palacios Francisco¹,Zuazua Enrique²

Affiliation:

1. Technical University of Madrid

2. Basque Center for Applied Mathematics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1299

Reference33 articles.

1. Airfoil Design on Unstructured Grids for Turbulent Flows

2. The ball-vertex method: a new simple spring analogy method for unstructured dynamic meshes

3. Systematic Continuous Adjoint Approach to Viscous Aerodynamic Design on Unstructured Grids

4. 5P. Cook, M. McDonald, and M. Firmin. Aerofoil rae2822 pressure distributions, and boundary layer and wake measurements. Technical Report AGARD 138, 1979.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Automatic differentiation based discrete adjoint method for aerodynamic design optimization on unstructured meshes;Chinese Journal of Aeronautics;2017-04

2. Robust Grid Adaptation for Efficient Uncertainty Quantification;AIAA Journal;2012-07

3. Adjoint-based method for supersonic aircraft design using equivalent area distribution;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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