Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages

被引：10
|
作者：
Trebinjac, I. [1 ]
Charbonnier, D. [1 ]
Leboeuf, F. [1 ]
机构：
[1] Ecole Cent Lyon, Lab Mecan Fluides & Acoust, CNRS, UMR 5509, F-69134 Ecully, France
来源：
JOURNAL OF THERMAL SCIENCE | 2005年 / 14卷 / 04期
关键词：
unsteady aerodynamics; rotor stator interaction; deterministic stress;
D O I：
10.1007/s11630-005-0047-6
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
The blade row interaction can alter the time-mean flow and therefore be of interest for aerodynamic design analysis. Whereas results within low subsonic turbomachines are quite numerous in the literature, there have been far fewer works which give results of blade row interaction within high speed cases. Two cases are related in this paper. First, the effects of an incoming wake on the rotor flow field of a transonic compressor are analyzed. The blade row interaction proved to be positive regarding the total pressure ratio, but negative regarding the losses. The second case concerns a transonic turbine. Particular emphasis is placed on the assessment of the deterministic correlations included in the Averaged Passage Equation System.
引用
收藏
页码：289 / 297
页数：9
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