The Effects of Blade Passing on the Heat Transfer Coefficient of the Overtip Casing in a Transonic Turbine Stage
Author:
Affiliation:
1. Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough LE12 7TW, UK
2. Department of Engineering Science, University of Oxford, Oxford, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2776950/5942489/041009_1.pdf
Reference23 articles.
1. 2004, Turbine Blade Tip Design and Tip Clearance Treatment, von Karman Institute for Fluid Dynamics Lecture Series, T.Arts, ed., von Karman Institute for Fluid Dynamics, Brussels.
2. Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip-Clearance;Yamamoto;ASME J. Turbomach.
3. The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades;Heyes;ASME J. Turbomach.
4. Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models;Kim;ASME J. Turbomach.
5. Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade;Papa;ASME J. Turbomach.
Cited by 3 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. Numerical investigations of the 3D transonic field and heat transfer at the over-tip casing in a HP-turbine stage;Applied Thermal Engineering;2016-06
2. Improved Methodologies for Time-Resolved Heat Transfer Measurements, Demonstrated on an Unshrouded Transonic Turbine Casing;Journal of Turbomachinery;2016-05-17
3. Analysis of the Unsteady Overtip Casing Heat Transfer in a High Speed Turbine;Journal of Turbomachinery;2013-03-25
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