Analysis of Gas Turbine Rotor Blade Tip and Shroud Heat Transfer
Author:
Affiliation:
1. A.Y.T. Corporation, Brook Park, OH
2. NASA Lewis Research Center
Abstract
Publisher
American Society of Mechanical Engineers
Link
http://asmedigitalcollection.asme.org/GT/proceedings-pdf/doi/10.1115/96-GT-189/4215992/v004t09a018-96-gt-189.pdf
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4. The Effects of Blade Passing on the Heat Transfer Coefficient of the Overtip Casing in a Transonic Turbine Stage;Journal of Turbomachinery;2008-07-31
5. Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade;International Journal of Heat and Mass Transfer;2004-12
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