Quantification of airfoil aerodynamic uncertainty due to pressure-sensitive paint thickness

Liu, S., Wang, Y., Qin, N. orcid.org/0000-0002-6437-9027 et al. (1 more author) (2019) Quantification of airfoil aerodynamic uncertainty due to pressure-sensitive paint thickness. AIAA Journal. ISSN 0001-1452

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2019 N Qin and SY Liu. This is an author-produced version of a paper subsequently published in AIAA Journal. Uploaded in accordance with the publisher's self-archiving policy.
Dates:
  • Accepted: 30 October 2019
  • Published (online): 27 November 2019
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: 12 Dec 2019 10:10
Last Modified: 13 Dec 2019 03:00
Status: Published online
Publisher: American Institute of Aeronautics and Astronautics (AIAA)
Refereed: Yes
Identification Number: https://doi.org/10.2514/1.j058801

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