Time-Averaged and Time-Accurate Aero-Dynamics for the Recessed Tip Cavity of a High-Pressure Turbine Blade and Outer Stationary Shroud: Comparison of Computational and Experimental Results.

Time-Averaged and Time-Accurate Aero-Dynamics for the Recessed Tip Cavity of a High-Pressure Turbine Blade and Outer Stationary Shroud: Comparison of Computational and Experimental Results.

Author(s):

Publication title:

A.S.M.E. paper

Title of ser.:

ASME Technical Paper : GT

Ser. no.:

2004

Pub. Year:

2004

No.:

GT2004-53443

Paper no.:

GT2004-53443

Pages:

16

Pub. info.:

New York, NY: American Society of Mechanical Engineers

Language:

English

Call no.:

A11800

Type:

Technical Paper

Details

TDL ID:	ZA00001648
Series ID:	PA00000136
Conf. info. (Name):	Turbo Expo 2004
Conf. info. (Number):	2004
Conf. info. (Venue):	Vienna, Austria
Conf. info. (Date):	2004.06.14-2004.06.17
Note for article:	Turbo Expo 2004, Vienna, Austria, 14-17 Jun. 2004

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