Direct Numerical Simulations of a High-Pressure Turbine Vane
Author:
Affiliation:
1. Whittle Laboratory, University of Cambridge, Cambridge CB3 0DY, UK e-mail:
2. Engineering and the Environment, University of Southampton, Southampton So17 1BJ, UK
3. GE Global Research, Munich D-85748, Germany
4. GE Aviation, Lynn, MA 01905
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4032435/6304294/turbo_138_07_071003.pdf
Reference39 articles.
1. Heat Transfer Optimized Turbine Rotor Blades—An Experimental Study Using Transient Techniques;ASME J. Eng. Gas Turbines Power,1984
2. Short Duration Measurements of Heat Transfer Rate to a Gas Turbine Rotor Blade;J. Eng. Power,1982
3. The Role of Laminar-Turbulent Transition in Gas Turbine Engines;ASME J. Turbomach.,1991
4. The Effects of Inlet Turbulence and Rotor/Stator Interactions on Aerodynamics and Heat Transfer of a Large-Scale Rotating Turbine Model,1986
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