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

Hinchliffe, B.L. and Qin, N. orcid.org/0000-0002-6437-9027 (2016) Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction. In: 54th AIAA Aerospace Sciences Meeting. 54th AIAA Aerospace Sciences Meeting, 04-08 Jan 2016, San Diego, CA. AIAA .

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2016 AIAA. This is an author produced version of a paper subsequently published in AIAA SciTech Forum. Uploaded in accordance with the publisher's self-archiving policy.
Dates:
  • Published: 4 January 2016
  • Accepted: 4 January 2016
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Funding Information:
FunderGrant number
AIRBUS UK LIMITED1100073482
AIRBUS UK LIMITEDAI-ECM090883
Depositing User: Symplectic Sheffield
Date Deposited: 15 Nov 2016 15:01
Last Modified: 21 Mar 2018 18:07
Published Version: https://doi.org/10.2514/6.2016-0560
Status: Published
Publisher: AIAA
Refereed: Yes
Identification Number: https://doi.org/10.2514/6.2016-0560

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