| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1562146 | Computational Materials Science | 2011 | 10 Pages |
Abstract
The present paper deals with the solution of the transient temperature transfer problem in bare and thermal barrier coated alloy Inconel 713 for the temperature range up to 1000 °C. The computational fluid dynamics (CFD) part of analysis was performed by application of ANSYS Fluent code receiving the temperature field of combustion gas, whereas computational structural mechanics (CMS) part concerning the temperature distribution inside the turbine blade was done by ABAQUS. Finally, the efficiency of the TBC layer (0.5 mm thickness) protecting and cooling channels was discussed in order to explore the operational temperature increase in the aero-engines.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
T. Sadowski, P. Golewski,