Investigating the Application of a Honeycomb Abradable Lining in the Turbine Stage of an Aero-Engine

Zhang, B. and Marshall, M.B. (2018) Investigating the Application of a Honeycomb Abradable Lining in the Turbine Stage of an Aero-Engine. Tribology International, 125. pp. 66-74. ISSN 0301-679X

Abstract

Metadata

Authors/Creators:
  • Zhang, B.
  • Marshall, M.B.
Copyright, Publisher and Additional Information: © 2018 Elsevier Ltd. This is an author produced version of a paper subsequently published in Tribology International. Uploaded in accordance with the publisher's self-archiving policy. Article available under the terms of the CC-BY-NC-ND licence (https://creativecommons.org/licenses/by-nc-nd/4.0/)
Dates:
  • Accepted: 11 April 2018
  • Published (online): 21 April 2018
  • Published: September 2018
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Funding Information:
FunderGrant number
ROLLS-ROYCE PLC4600133549 - 4600133119
ENGINEERING AND PHYSICAL SCIENCE RESEARCH COUNCIL (EPSRC)EP/H023895/1
ROLLS-ROYCE PLC4600133549 - 4600133119
ROLLS-ROYCE PLC5003523553
ROLLS-ROYCE PLC1500-00006619
Depositing User: Symplectic Sheffield
Date Deposited: 24 Apr 2018 15:39
Last Modified: 21 Apr 2019 00:43
Published Version: https://doi.org/10.1016/j.triboint.2018.04.013
Status: Published
Publisher: Elsevier
Refereed: Yes
Identification Number: https://doi.org/10.1016/j.triboint.2018.04.013

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