The effect of hub leakage flow on two high speed axial flow compressor rotors

The effect of hub leakage flow on two high speed axial flow compressor rotors

Author(s):

Shabbir, A. ( NASA Lewis Research Center )
Celestina, M.L.
Adamczyk, J.J.
Strazisar, A.J.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1997

Pub. Year:

1997

No.:

97-GT-346

Paper no.:

97-GT-346

Pub. info.:

New York: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002614
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine & Aeroengine Congress & Exhibition
Conf. info. (Number):	1997
Conf. info. (Venue):	Orlando, Florida
Conf. info. (Date):	1997.06.02-1997.06.05
Note for article:	Presented at the International Gas Turbine & Aeroengine Congress & Exhibition Orlando, Florida - June 2-June 5, 1997

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