Experimental and numerical flow visualization in a transonic turbine

被引:8
|
作者
Woisetschlager, J. [1 ]
Pecnik, R. [1 ]
Goethch, E. [1 ]
Schennach, O. [1 ]
Marn, A. [1 ]
Sanz, W. [1 ]
Heitmeir, F. [1 ]
机构
[1] Graz Univ Technol, Inst Thermal Trubomachinery & Machine Dynam, A-8010 Graz, Austria
基金
奥地利科学基金会;
关键词
Particle Image Velocimetry; turbomachinery; transonic flow; blade row interaction; computational fluid dynamics;
D O I
10.1007/BF03181919
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper focuses on the visualization of both experimental and numerical results and presents research in a highly-loaded cold-flow transonic turbine under continuous and engine-representative conditions. Special focus was placed on blade row interaction at app. 10600 rpm. While the first step was the investigation of a single stage machine (stator-rotor), the second step extended the test rig to a one-and-a-half stage configuration (stator-rotor-stator). Measurements were carried out in the transonic test turbine at Graz University of Technology using Particle-Image-Velocimetry and Laser-Doppler-Anemometry. The main results of these experiments are discussed and compared to numerical simulations.
引用
收藏
页码:95 / 102
页数:8
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