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

Journal article

Peer reviewed

Journal of Engineering for Gas Turbines and Power: Transactions of the ASME

01/07/2015

Abstract

coupled aero-thermal modeling

aero-engine compressor disc cavity

radial inflow

thermal response time

blade tip clearance control

url

http://gasturbinespower.asmedigitalcollection.asme.org/journal.aspxView

Published (Version of record)

Title: Coupled Aero-Thermal Modeling of a Rotating Cavity with Radial Inflow
Creators: Zhili Sun
Dario Amirante
John Chew
Nicholas Hills
Publication Details: Journal of Engineering for Gas Turbines and Power: Transactions of the ASME
Publisher: ASME
Publication Date: 01/07/2015
Identifiers: 99515427602346
Academic Unit: School of Mechanical Engineering Sciences
Resource Type: Journal article