英语语法分析

Structural reliability analysis of an aeroengine 2nd-stage compressor disk is presented.

对某型发动机压气机第2级轮盘进行了结构可靠性分析。

Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.

低循环多轴疲劳失效是航空发动机低压压气机轮盘的主要失效形式。

The establishment and existing problems of metallurgy model standard for an aeroengine are introduced.

介绍了某型航空发动机冶金型号标准的编制情况及其尚存在的问题。