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International Journal of Rotating Machinery
Volume 8, Issue 2, Pages 81-86

Theoretical Analysis of Heat Transfer Through an Idealized Gas Turbine Blade Model with Thermal Barrier Coating

1Department of Mechanical Engineering and Applied Mechanics, The University of Michigan, Ann Arbor 48109, Michigan, USA
2R & D Divison, Noritake Co. Ltd., Aichi, Japan
3Research Center for Advanced Energy Conversion, Nagoya University, Nagoya, Japan
4Karadeniz Technical University, Trabzon 61080, Turkey

Copyright © 2002 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


This article has no abstract.