Leading edge film cooling of a turbine blade model through single and double row injection: Effects of coolant density

Leading edge film cooling of a turbine blade model through single and double row injection: Effects of coolant density

Author(s):

Salcudean, M. ( University of British Columbia )
Gartshore, I.
Zhang, K.
Barnea, Y.

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Pub. Year:

1994

No.:

94-GT-2

Paper no.:

94-GT-2

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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