Heat transfer and flow on the first stage blade tip of a power generation gas turbine. Part 2, Simulation results /

"A combined experimental and computational study has been performed to investigate the detailed distribution of convective heat transfer coefficients on the first stage blade tip surface for a geometry typical of large power generation turbines (>100MW). This paper is concerned with the nume...

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Bibliographic Details

Main Author:	Ameri, Ali A.
Corporate Authors:	NASA Glenn Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Bunker, Ronald S.
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [1999]
Series:	NASA contractor report ; NASA CR-209151.
Subjects:	Gas-turbines > Blades. Heat > Transmission. Mathematical models.
Online Access:	http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990047910_1999064385.pdf