摘要
本文介绍了某型高压涡轮级气动特性试验结果,主要包括总性能、变冷气流量比性能和变转子叶尖间隙性能三部分,并对此进行了分析。
This paper introduced the experimental results of aerodynamic performance test of a highpressure turbine. The results included three parts： the total performance, the performance with changing cooling air flow ratio and the performance with changing rotor blade tip clearance.
出处
《燃气涡轮试验与研究》
2005年第4期20-23,29,共5页
Gas Turbine Experiment and Research
关键词
涡轮
气动特性
试验研究
turbine
aerodynamic performance
experimental study
