TEMPERATURE DISTRIBUTION IN MULTILAYER METAL-CERAMIC COATINGS UNDER NONSTATIONARY THERMAL EFFECTS

TEMPERATURE DISTRIBUTION IN MULTILAYER METAL-CERAMIC COATINGS UNDER NONSTATIONARY THERMAL EFFECTS

Progress in the aircraft engine construction is determined by the increase of operation parameters of gas turbine engines, which is inevitably accompanied by an increase of operating temperatures and load for the vital elements of the turbine hot ducts. Furthermore, the requirements for reliability...

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Bibliographic Details
Main Authors:	V. M. Samoilenko, Y. V. Petrov, O. A. Ratenko
Format:	Article
Language:	Russian
Published:	Moscow State Technical University of Civil Aviation 2017-09-01
Series:	Naučnyj Vestnik MGTU GA
Subjects:	turbine blade combined heat-resistant coating thermal conductivity durability serviceability
Online Access:	https://avia.mstuca.ru/jour/article/view/1116

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