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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| 格式: | 文件 |
| 语言: | Russian |
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Moscow State Technical University of Civil Aviation
2017-09-01
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| 丛编: | Научный вестник МГТУ ГА |
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| 在线阅读: | https://avia.mstuca.ru/jour/article/view/1116 |