Application of Nonaxisymmetric Endwall Contouring to Conventional and High-Lift Turbine Airfoils
Author:
Affiliation:
1. Aerodynamics Group, United Technologies, Pratt & Whitney, East Hartford, CT 06108
2. Department of Mechanical and Aerospace Engineering, Carleton University, Ottawa, ON, K1S 5B6, Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4024023/6295640/turb_135_06_061006.pdf
Reference35 articles.
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2. Three-Dimensional Flow Within a Turbine Cascade Passage,1976
3. Recent Progress in the Understanding of Basic Aspects of Secondary Flows in Turbine Blade Passages;ASME J. Eng. Power,1985
4. Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades;ASME J. Turbomach.,1987
5. The Application of Ultra-High Lift Blading in the BR715 LP Turbine,2001
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