Theoretical Analysis of Heat Transfer Through an Idealized Gas Turbine Blade Model with Thermal Barrier Coating
Saved in:
| Main Authors: | Aydin Orhan, Iwata Misao, Arai Noroi, Yang Wen-Jei |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2002-01-01
|
| Series: | International Journal of Rotating Machinery |
| Online Access: | http://www.hindawi.net/access/get.aspx?journal=ijrm&volume=8&pii=S1023621X02000088 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Deterioration of Thermal Barrier Coated Turbine Blades by Erosion
by: Rohan Swar, et al.
Published: (2012-01-01) -
Furnace Testing and Validation of a Hybrid Cooling Approach for Enhanced Turbine Blade Protection with a Thermal Barrier Coating in Advanced Gas Turbines
by: Salmi Mohd Yunus, et al.
Published: (2024-09-01) -
EVALUATION OF OPERATIONAL EFFICIENCY OF DIFFUSION COATINGS FOR TURBINE BLADES OF CONTEMPORARY GAS TURBINE ENGINES
by: E. G. Ivanov, et al.
Published: (2016-11-01) -
Vacuum-plasma protective coating for turbines blades.
by: O. V. Sagalovych, et al.
Published: (2020-04-01) -
Evolution of Rotating Internal Channel for Heat Transfer Enhancement in a Gas Turbine Blade
by: Xinxin Guo, et al.
Published: (2024-10-01)