This study is of significance to the technological design in the compressorstator blade forging process.
该研究对压气机静子叶片锻造工艺的优化设计具有重要的指导意义。
2
Characteristics of honeycomb structures of compressorstator and combustion chamber are narrated and studied also for their repairing processes.
叙述了压气机静子蜂窝封严扇形段和燃烧室前封严环组件的结构特点,对蜂窝组件的修理过程进行了研究。
3
Based on a high-accuracy and large-scale-parallel method, SA model and detached eddy simulation (DES) based on SA were employed to research the flows of compressorstator-rotor interaction.