The effect of airfoil scaling on the predicted unsteady loading on the blade of a 1 and 1/2 stage transonic turbine and a comparison with experimental results

The effect of airfoil scaling on the predicted unsteady loading on the blade of a 1 and 1/2 stage transonic turbine and a comparison with experimental results

Author(s):

Clark, J. P. ( United Technologies Pratt & Whitney )

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-GT-446

Paper no.:

2000-GT-446

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 Turbine & Aeroengine Congress & Exhibition Munich, Germany-May 8-11, 2000

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