Modelling roughness effects for transitional low Reynolds number aerofoil flows

Liu, S. and Qin, N. (2014) Modelling roughness effects for transitional low Reynolds number aerofoil flows. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229 (2). 280 - 289. ISSN 0954-4100

Abstract

Metadata

Authors/Creators:
  • Liu, S.
  • Qin, N.
Copyright, Publisher and Additional Information: © 2014 SAGE Publications. This is an author produced version of a paper subsequently published in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: Low Reynolds number; roughness effects; transition modelling; micro air vehicles; computational fluid dynamics
Dates:
  • Published: 8 April 2014
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 16:49
Last Modified: 03 Nov 2016 09:24
Published Version: https://doi.org/10.1177/0954410014530875
Status: Published
Publisher: SAGE Publications
Refereed: Yes
Identification Number: https://doi.org/10.1177/0954410014530875
Related URLs:

Download not available

A full text copy of this item is not currently available from White Rose Research Online

Export

Statistics