Aeromechanical Optimization of a Winglet-Squealer Tip for an Axial Turbine
Author:
Affiliation:
1. Whittle Laboratory, University of Cambridge, Cambridge CB3 0DY, UK
2. Rolls-Royce Plc., P.O. Box 31, Derby DE24 8BJ, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4025687/6299114/turb_136_07_071004.pdf
Reference20 articles.
1. Hourmouziadis, J., and Albrecht, G., 1987, “An Integrated Aero/Mechanical Performance Approach to High Technology Turbine Design,” Paper No. AGARD-CP-421.
2. Denton J.D. , 1993, “Loss Mechanisms in Turbomachines,” ASME Paper No. 93-GT-435.
3. Sjolander, S.A., and Cao, D., 1994, “Measurements of the Flow in an Idealized Turbine Tip Gap,” ASME Paper No. 94-GT-74.
4. Measurement and Prediction of Tip Clearance Flow in Linear Turbine Cascades;ASME J. Turbomach.,1993
5. Booth, T.C., Dodge, P.R., and Hepworth, H.K., 1981, “Rotor-Tip Leakage Part I—Basic Methodology,” ASME Paper No. 81-GT-71.
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