University of Surrey

Test tubes in the lab Research in the ATI Dance Research

Coupled Aero-Thermal Modeling of a Rotating Cavity with Radial Inflow

Sun, Z, Amirante, D, Chew, J and Hills, NJ (2015) Coupled Aero-Thermal Modeling of a Rotating Cavity with Radial Inflow Journal of Engineering for Gas Turbines and Power: Transactions of the ASME.

[img]
Preview
Text
GTP-15-1298 final.pdf
Available under License : See the attached licence file.

Download (2MB) | Preview
[img]
Preview
Text (licence)
SRI_deposit_agreement.pdf
Available under License : See the attached licence file.

Download (33kB) | Preview
Item Type: Article
Divisions : Faculty of Engineering and Physical Sciences > Mechanical Engineering Sciences
Authors :
AuthorsEmailORCID
Sun, ZUNSPECIFIEDUNSPECIFIED
Amirante, DUNSPECIFIEDUNSPECIFIED
Chew, JUNSPECIFIEDUNSPECIFIED
Hills, NJUNSPECIFIEDUNSPECIFIED
Date : 1 July 2015
Uncontrolled Keywords : coupled aero-thermal modeling, aero-engine compressor disc cavity, radial inflow, thermal response time, blade tip clearance control
Additional Information : Copyright 2015 ASME. Paper accepted for publication in Journal of Engineering for Gas Turbines and Power: Transactions of the ASME.
Depositing User : Symplectic Elements
Date Deposited : 14 Aug 2015 10:57
Last Modified : 14 Aug 2015 10:57
URI: http://epubs.surrey.ac.uk/id/eprint/808245

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year


Information about this web site

© The University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom.
+44 (0)1483 300800