Measurements of Secondary Flows in a Turbine Cascade at Off-Design Incidence

Author:

Benner M. W.1,Sjolander S. A.1,Moustapha S. H.2

Affiliation:

1. Carleton University, Ottawa, ON, Canada

2. Pratt & Whitney Canada Inc., Longueuil, QC, Canada

Abstract

The present study is part of an on-going project concerned with the effects of off-design incidence on losses. Previous work has examined the profile losses (Benner et al., 1995). This study focusses on the secondary flow, the endwall flow in the absence of tip clearance. This paper describes an experimental study in a large-scale, low-speed, linear turbine cascade for which the incidence was varied. Three different values of incidence were investigated: 0, +10 and +20 degrees. Detailed flow field measurements were made upstream and downstream of the cascade and static pressure distributions were measured on the blade surfaces. The data were supplemented by extensive surface oil flow visualization. This paper concentrates on the physical insights into the relationship between the behaviour of secondary flows and incidence which have been gained from the measurements and the flow visualization. A preliminary discussion of the effect of incidence on the losses is also included.

Publisher

American Society of Mechanical Engineers

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Stationary and Traveling Vortical Structures on Swept Cylinders and Turbine Blades;43rd Fluid Dynamics Conference;2013-06-22

2. Streamwise Vorticity, Laminar Separation and Transition in Flows over Turbomachinery Blades;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

3. Organized Streamwise Vorticity on Convex Surfaces With Particular Reference to Turbine Blades;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

4. An Empirical Prediction Method for Secondary Losses in Turbines—Part I: A New Loss Breakdown Scheme and Penetration Depth Correlation;Journal of Turbomachinery;2005-02-01

5. The Influence of Leading-Edge Geometry on Secondary Losses in a Turbine Cascade at the Design Incidence;Journal of Turbomachinery;2004-04-01

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