Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction-Reference-Cited by-同舟云学术

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Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Hinchliffe Benjamin L.¹,Qin Ning¹

Affiliation:

1. University of Sheffield

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0560

Reference38 articles.

1. Report 93025 DERA, May 1993.

2. 3Fulker, J. L., Ashilll, P. R., and Simmons, M. J. “Computational Study of Shock Control at Transonic Speed,” PhD Thesis,

3. Cranfield University, 2000.

4. 4Lutz, T., Kutzbach, M., and Wagner, S. “Investigations on shock control bumps for infinite swept wings,” AIAA 2004-2702 ,

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. Towards a Framework for Parametric Models and Geometric Sensitivity Computations with SU2 and pyCAPS;AIAA AVIATION 2023 Forum;2023-06-08

2. Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction;AIAA Journal;2017-03

3. Effect of Non-Consistent Mesh Movements and Sensitivities on a Discrete Adjoint Based Aerodynamic Optimization;55th AIAA Aerospace Sciences Meeting;2017-01-05

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