A Three-Dimensional Coupled Internal/External Simulation of a Film-Cooled Turbine Vane
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, OH
2. Dynacs Engineering Co., Inc., Brookpark, OH
3. AYT Corporation, Cleveland, OH
Abstract
Publisher
American Society of Mechanical Engineers
Link
http://asmedigitalcollection.asme.org/GT/proceedings-pdf/doi/10.1115/99-GT-186/2412214/v003t01a053-99-gt-186.pdf
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1. Numerical investigation of internal crossflow effects on film cooling performance at turbine blade suction surface;Journal of Thermal Science and Technology;2018
2. Conjugate calculation of a film-cooled blade for improvement of the leading edge cooling configuration;Propulsion and Power Research;2013-03
3. An Investigation of Treating Adiabatic Wall Temperature as the Driving Temperature in Film Cooling Studies;Journal of Turbomachinery;2012-09-17
4. CFD Simulations Using Reduced Models for Film Cooling Design;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
5. Multi-Physics CFD Simulations on Heat and Fluid Flow Phenomena with Sand Transfer(The Forefront of Multi-Physics CFD/EFD);Transactions of the Japan Society of Mechanical Engineers Series B;2010
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