AN EXPERIMENTAL CONVECTIVE HEAT-TRANSFER INVESTIGATION AROUND A FILM-COOLED GAS-TURBINE BLADE

被引:44
作者
CAMCI, C
ARTS, T
机构
[1] Aerospace Engineering Department, The Pennsylvania State University, University Park, PA
[2] Von Karman Institute for Fluid Dynamics, Rhode Saint Genese, Rhode Saint Genáse
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1990年 / 112卷 / 03期
关键词
D O I
10.1115/1.2927685
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The present paper deals with an experimental convective heat transfer investigation around a film-cooled, high-pressure gas turbine rotor blade mounted in a stationary, linear cascade arrangement. The measurements were performed in the von Karman Institute Isentropic Light Piston Compression Tube facility. The test blade was made of Macor glass ceramic and was instrumented with thin film gages. The coolant flow was ejected simultaneously through the leading edge (three rows of holes), the suction side (two rows of holes), and the pressure side (one row of holes). The effects of overall mass weight ratio, coolant to free-stream temperature ratio, and free-stream turbulence were successively investigated. © 1990 by ASME.
引用
收藏
页码:497 / 503
页数:7
相关论文
共 19 条
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