Effect of stator design on stator boundary layer flow in a highly loaded single-stage axial-flow low-speed compressor

Effect of stator design on stator boundary layer flow in a highly loaded single-stage axial-flow low-speed compressor

Author(s):

Friedrichs, Jens ( Pfleiderer-Institute TU Braunshweig )
Kosyna, Gunter
Baumgarten, Sven
Stark, Udo

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-GT-616

Paper no.:

2000-GT-616

Pub. info.:

New York: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00001744
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine and Aeroengine Congress & Exhibition
Conf. info. (Number):	2000
Conf. info. (Venue):	Munich, Germany
Conf. info. (Date):	2000.05.08-2000.05.11
Note for article:	Presented at the International Gas Turbin & Aeroengine Congress & Exhibition Munich, Germany - May 8-11, 2000 This paper has been accepted for publication in the Transactions of the ASME Discussion of it will be accepted at ASME Headquarters until August 30, 2000

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