Lv11
40 积分 2025-02-05 加入
Study on the flow mechanism of turbine blades considering combustor exit swirling flow
1小时前
求助中
The icing characteristic of stage 35 compressor blades and its impact on aerodynamic performance
9个月前
已完结
System Level Analysis of Compressor Eye-Labyrinth Seal Rotordynamic Forces: A Computational Fluid Dynamics Approach
10个月前
已完结
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