Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance of a Low Speed Compressor Rotor

Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance of a Low Speed Compressor Rotor

Author(s):

Daniel Lee

Publication title:

Turbomachinery, Parts A, B, and C; Volume 6

Title of ser.:

ASME Symposia Volumes

Ser. no.:

TURBO EXPO 2008(6A)

Pub. Year:

2008

Vol.:

6A

Paper no.:

GT2008-51385

Page(from):

681

Page(to):

694

Pages:

14

Pub. info.:

New York: American Society of Mechanical Engineers

ISBN:

9780791843161 [0791843165]

Language:

English

Call no.:

A11661/2008

Type:

Conference Proceedings

Details

TDL ID:	ZA00049427
Series ID:	PA00000270
Conf. info. (Name):	ASME Turbo Expo : Power for Land, Sea, and Air
Conf. info. (Number):	2008
Conf. info. (Venue):	Berlin, Germany
Conf. info. (Date):	2008.06.09-2008.06.13

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