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：
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页码：1125 / 1129
页数：4
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