欢迎您！东篱公司
退出
-
申报数据库
-
立项数据库
-
成果数据库
-
项目获奖数据库
中文摘要：
本文分别以一个低压比和一个高压比离心叶轮为对象，采用FINE／TURBO软件包，数值分析了叶片根部加倒角对叶轮流场气动性能的影响。结果表明；叶根倒角的存在会使流量减小，倒角越大，通流量也越小；倒角使压比和效率均有所下降，并对叶根附近流动参数分布带来明显的影响。
英文摘要：
Taking two kinds of centrifugal compressor impellers with low and high pressure ratios, respectively, this paper studies the influence of root fillet on the aerodynamic performance of centrifugal impellers by using a commercial software FINETg/Turbo. The results show that a blade with root fillet would reduce the mass flow, and the bigger the fillet, the smaller the mass. Due to the fillet, pressure ratio and efficiency would also be declined. However, influence on the 3D flow is only significant near the root range.
同期刊论文项目
同项目期刊论文
Influence of shock systems on suction surface film cooling in turbine convergent-divergent-nozzle ro
Tip clearance effects on inlet hot streak migration characteristics in high pressure stage of a vane
An investigation on aerodynamic performance of a vaneless counter-rotating turbine with recessed hig
Experimental investigation on unsteady pressure fluctuation of rotor tip region in high pressure sta
Tip-Clearance Effects on Hot-Streak Migration in Low-Pressure Stage of Vaneless Counter-Rotating Tur
Numerical simulation of shock systems in converging-diverging nozzle rotor turbine stage with differ
Investigation of influencing factors of hot streaks migration in high pressure stage of a vaneless c
Discussion on the feasibility of CFD application in the estimation of wind speed distribution in a w
期刊信息
位置：