APPLICATION OF MATHEMATICAL SIMULATION TO CHOOSE THE COMPOSITION OF THE THERMAL PROTECTION COATING OF UNDERLAYER

The article considers the use of mathematical modeling while designing thermal protection coating for GTE turbine blades. The results of mathematical simulation are presented and comparison with experimental data is given. The obtained results allow to choose the composition of a underlayer to cover...

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Bibliographic Details
Main Authors: A. M. Amouei, G. R. Mirhosseini, A. Jafari, M. Saadatibaei
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-12-01
Series:Научный вестник МГТУ ГА
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/866
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