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):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2008

Pub. Year:

2008

No.:

GT2008-51385

Paper no.:

GT2008-51385

Pages:

14

Pub. info.:

New York, NY: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00052167
Series ID:	PA00000136
Conf. info. (Name):	ASME Turbo Expo 2007: Power for Land, Sea and Air
Conf. info. (Number):	2008
Conf. info. (Venue):	Berlin, Germany
Conf. info. (Date):	2008.06.09-2008.06.13
Note for article:	ASME Turbo Expo 2008: Power for Land, Sea and Air, Berlin, Germany, 2008.06.09-2008.06.13

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