Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation

Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation

Author(s):

Moyle, I. N. ( Naval Postgraduate School )
Walker, G. J.
Shreeve, R. P.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1991

Pub. Year:

1991

No.:

91-GT-30

Paper no.:

91-GT-30

Pub. info.:

New York, NY: The American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00002837
Series ID:	PA00000136
Conf. info. (Name):	International Gas Turbine and Aeroengine Congress and Exposition
Conf. info. (Number):	1991
Conf. info. (Venue):	Orlando, FL
Conf. info. (Date):	1991.06.03-1991.06.06
Note for article:	Presented at the International Gas Turbine and Aeroengine Congress and Exposition Orlando, FL June 3-6, 1991 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, 1991

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