离散气膜孔对涡轮端壁气膜冷却特性的影响

Translated title of the contribution: Effect of Discrete Film holes on Film Cooling Characteristic of a Turbine Endwall

Jie Zhang, Cunliang Liu, Xiying Niu, Lin Ye, Li Zhang

Research output: Contribution to journalArticlepeer-review

Abstract

In this paper, the effects of mass flow ratio, density ratio and leakage flow on the film cooling characteristic of the turbine endwall with a discrete film hole layout were studied using the pressure sensitive paint (PSP) technology. The results show that the mass flow ratio of the discrete film holes (Rmf1) has a great influence on the distribution of film cooling effectiveness in the upstream region of the endwall, especially the area near the pressure side. As the density ratio (Rd) increases, the film cooling effectiveness in the upstream region of the endwall is gradually improved, however, the effect of the Rd on the film cooling in the downstream region of the endwall is reduced due to the intensity of the passage vortex quickly increases along the mainflow direction. In addition, the leakage flow greatly improves the average surface film cooling effectiveness of the endwall, particularly when Rmf1=1.75%, the average surface cooling effectiveness is increased by 77.8%.

Translated title of the contributionEffect of Discrete Film holes on Film Cooling Characteristic of a Turbine Endwall
Original languageChinese (Traditional)
Pages (from-to)3331-3337
Number of pages7
JournalKung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
Volume45
Issue number11
StatePublished - Nov 2024

Fingerprint

Dive into the research topics of 'Effect of Discrete Film holes on Film Cooling Characteristic of a Turbine Endwall'. Together they form a unique fingerprint.

Cite this