The effect of blade tip geometry on the tip leakage flow in axial turbine cascades

The effect of blade tip geometry on the tip leakage flow in axial turbine cascades

Author(s):

Heyes, F. J. G. ( Cambridge University )
Hodson, H. P.
Dailey, G. M.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1991

Pub. Year:

1991

No.:

91-GT-135

Paper no.:

91-GT-135

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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