Effect of Rotor Tip Gap Variation at the Rear Stages of an Axial Flow Compressor
Conference; 4th, AEROTECH IV - recent advances in aerospace technologies: selected, peer reviewed papers from the AEROTECH IV, November 21-22, 2012, Kuala Lumpur, Malaysia / ; 2012 ; Kuala Lumpur
2012-01-01
6 pages
Includes bibliographical references and index.
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Axial Compressor Rotor Flow Structure at Stall-Inception
AIAA | 2006
|Inverse design of the blading of subsequent axial flow compressor stages
Online Contents | 1996
|Behaviour of tip-leakage flow in an axial flow compressor rotor
Online Contents | 2007
|