Transonic Turbine Stage Heat Transfer Investigation in Presence of Strong Shocks
Author:
Affiliation:
1. Turbomachinery and Propulsion Department, von Karman Institute, Rhode Saint Genèse B1640, Belgium
2. Energy Department “Sergio Stecco,” University of Florence, Florence 50139, Italy
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2777193/5843539/031019_1.pdf
Reference33 articles.
1. Aero-Thermal Performance of a Two-Dimensional Highly Loaded Transonic Turbine Nozzle Guide Vane: A Test Case for Inviscid and Viscous Flow Computations;Arts;ASME J. Turbomach.
2. Aero-Thermal Performance Measurements and Analysis of a Two-Dimensional High Turning Rotor Blade;Arts;ASME J. Turbomach.
3. Popp, O. , 1999, “Steady and Unsteady Heat Transfer in a Film Cooled Transonic Turbine Cascade,” Doctoral Dissertation, Virginia Polytechnic Institute∕Virginia State University, Blacksburg, VA.
4. Giel, P. W., Van Fossen, G. J., Boyle, R. J., Thurman, D. R., and Civinskas, K. C., 1999, “Blade Heat Transfer Measurements and Predictions in a Transonic Turbine Cascade,” ASME Paper No. 99-GT-125.
5. Sieverding, C. H., and Arts, T., 1992, “The VKI Compression Tube Annular Cascade Facility CT3,” ASME Paper No. 92-GT-336.
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