APPLICATION OF MATHEMATICAL SIMULATION TO CHOOSE THE COMPOSITION OF THE THERMAL PROTECTION COATING OF UNDERLAYER
Abstract
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 the metal layer of thermal protection coating.
About the Authors
A. M. AmoueiRussian Federation
G. R. Mirhosseini
Russian Federation
A. Jafari
Russian Federation
M. Saadatibaei
Russian Federation
References
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Review
For citations:
Amouei A.M., Mirhosseini G.R., Jafari A., Saadatibaei M. APPLICATION OF MATHEMATICAL SIMULATION TO CHOOSE THE COMPOSITION OF THE THERMAL PROTECTION COATING OF UNDERLAYER. Civil Aviation High Technologies. 2016;(225):9-13. (In Russ.)
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