Lv1
50 积分 2025-10-09 加入
Effect of blade squealer tips on aerodynamic performance and stall margin in a transonic centrifugal compressor with vaned diffuser
5个月前
已完结
Experiment Investigation on Secondary Flow Loss and Flow Control Mechanisms in a Variable Compressor Cascade with Penny Cavities
7个月前
已完结
Mechanism of effects of adjustable stator clearances axial location on a high-load axial flow compressor performance
7个月前
已完结
皖公网安备34019202002308
