Fine grain cast IN718 compressor blade form abroad has been analyzed.
解剖、分析了国外细晶铸造IN718压气机叶片。
The failure characteristics of compressor blade break at dovetail position. are introduced in this paper.
阐明了某机第4级压气机转子叶片在榫头部位断裂的故障特点。
But the aerodynamic optimization of the turbomachinery blade, especially the transonic compressor blade, is still a challenge area.
但是叶轮机械,尤其是跨音速轴流压气机叶片的气动优化设计仍然是一个具有挑战性的研究领域。
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