Heat transfer on a film-cooled rotating blade [microform] / Vijay K. Garg.

"A multi-block, three-dimensional Navier-Stokes code has been used to compute heat transfer coefficient on the blade, hub and shroud for a rotating high-pressure turbine blade with 172 film-cooling holes in eight rows. Film cooling effectiveness is also computed on the adiabatic blade. Wilcox&#...

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Bibliographic Details

Online Access:	Click here to view full text online
Main Author:	Garg, Vijay K., 1947-
Corporate Author:	NASA Glenn Research Center
Other title:	Heat transfer on a film cooled rotating blade.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], [1999]
Series:	NASA contractor report ; NASA CR-209301.
Subjects:	Heat > Transmission. Heat transfer. Heat transfer coefficients. Multiblock grids. Navier-Stokes equation. Three dimensional models. Film cooling. Turbulent flow. K-omega turbulence model. Computational fluid dynamics.