Physical phenomena in the polishing of compressor blades for gas-turbine engines

被引：0
|
作者：
V. F. Makarov
E. N. Bychina
机构：
[1] Perm State Technical University,
[2] Perm Engine Company OJSC,undefined
来源：
Russian Engineering Research | 2012年 / 32卷 / 2期
关键词：
Residual Stress; Titanium Alloy; RUSSIAN Engineer Research; Compressor Blade; Axial Residual Stress;
D O I：
10.3103/S1068798X12020207
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：203 / 206
页数：3
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