Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part I - A model for subsonic flow

Improved blade profile loss and deviation angle models for advanced transonic compressor bladings: Part I - A model for subsonic flow

Author(s):

Konig, W. M. ( Technical University of Darmstadt )
Hennecke, D. K.
Fottner, L.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Pub. Year:

1994

No.:

94-GT-335

Paper no.:

94-GT-335

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00005619
Series ID:	PA00000136
Note for article:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition The Hague, Netherlands - June 13-16, 1994 This paper has been accepted for publication in the Transactions of the ASME Discussion of it will be accepted at ASME Headquarters until September 30, 1994

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