Experimental investigation of a cooling system entrance for an annular gas turbine combustion chamber

Experimental investigation of a cooling system entrance for an annular gas turbine combustion chamber

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

1997

Pub. Year:

1997

No.:

97-GT-477

Paper no.:

97-GT-477

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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