Efficient BEM Modeling of the Heat Transfer in the Turbine Blades of Aero-Parts
The modeling of the turbine blades in aero-parts presents difficulties in conventional domain solution techniques, especially when internal cooling air passages and a thermal barrier coating (TBC) are applied. This paper presents a very efficient 3D modeling of the anisotropic heat conduction in tur...
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Published in | Aerospace Vol. 10; no. 10; p. 885 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Basel
MDPI AG
01.10.2023
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Subjects | |
Online Access | Get full text |
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