Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings

Zhu, F., Hinchliffe, B. and Qin, N. (2015) Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings. In: 53rd AIAA Aerospace Sciences Meeting. 53rd AIAA Aerospace Sciences Meeting, 5-9 January 2015, Kissimmee, Florida (USA). AIAA SciTech (1488). American Institute of Aeronautics and Astronautics (AIAA) . ISBN 978-1-62410-343-8

Abstract

Metadata

Authors/Creators:
  • Zhu, F.
  • Hinchliffe, B.
  • Qin, N.
Copyright, Publisher and Additional Information: © 2015 AIAA. This is an author produced version of a paper subsequently published in 53rd AIAA Aerospace Sciences Meeting. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: Aerodynamic optimisation; Adjoint method; Shock control bump; Transonic wing
Dates:
  • Published: January 2015
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Depositing User: Symplectic Sheffield
Date Deposited: 13 Oct 2015 16:40
Last Modified: 03 Nov 2016 09:26
Published Version: https://doi.org/10.2514/6.2015-1488
Status: Published
Publisher: American Institute of Aeronautics and Astronautics (AIAA)
Series Name: AIAA SciTech
Refereed: Yes
Identification Number: https://doi.org/10.2514/6.2015-1488

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