On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine.

On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine.

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-GT-197

Paper no.:

2001-GT-197

Pages:

10

Pub. info.:

New York, NY: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00001746
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine and Aeroengine Congress and Exhibition
Conf. info. (Number):	2001
Conf. info. (Venue):	New Orleans, LA
Conf. info. (Date):	2001.06.04-2001.06.07
Note for article:	International Gas Turbine and Aeroengine Congress and Exhibition, New Orleans, LA, 4-7 June 2001

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