Numerical simulation of aircraft thermal anti-icing system based on a tight-coupling method

Bu, X, Lin, G, Shen, X et al. (2 more authors) (2020) Numerical simulation of aircraft thermal anti-icing system based on a tight-coupling method. International Journal of Heat and Mass Transfer, 148. 119061. ISSN 0017-9310

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Copyright, Publisher and Additional Information: © 2019 Elsevier Ltd. All rights reserved. This is an author produced version of a paper published in International Journal of Heat and Mass Transfer. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: Aircraft icing; Conjugate heat transfer; Tight-coupling method; Electro-thermal anti-icing system; Numerical simulation
Dates:
  • Published: February 2020
  • Accepted: 14 November 2019
  • Published (online): 21 November 2019
Institution: The University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering (Leeds) > School of Chemical & Process Engineering (Leeds)
Depositing User: Symplectic Publications
Date Deposited: 06 Jan 2020 10:11
Last Modified: 06 Jan 2020 10:11
Status: Published
Publisher: Elsevier
Identification Number: https://doi.org/10.1016/j.ijheatmasstransfer.2019.119061

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Filename: AAV_buxueqinNumerical Simulation of Aircraft Thermal Anti-icing System.pdf

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