Technique for Estimating the Residual Life of Gas Turbine Engine Blades under High-Temperature Creep

被引：0

作者：

O. A. Ratenko

Yu. V. Petrov

V. M. Samoylenko

机构：

[1] Moscow State Technical University of Civil Aviation,

来源：

Russian Metallurgy (Metally) | 2022年 / 2022卷

关键词：

turbine blade; γ' phase; coagulation; microstructure;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：1125 / 1129

页数：4

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