Blockage Effects From Simulated Thermal Barrier Coatings for Cylindrical and Shaped Cooling Holes
Author:
Affiliation:
1. Mechanical and Nuclear Engineering Department, The Pennsylvania State University, University Park, PA 16802 e-mail:
2. Pratt & Whitney, 400 Main Street, East Hartford, CT 06118 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4029879/6302804/turbo_137_09_091004.pdf
Reference14 articles.
1. Bunker, R. J., 2000, “Effect of Partial Coating Blockage on Film Cooling Effectiveness,” ASME Paper No. 2000-GT-0244.10.1115/2000-GT-0244
2. Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness and Associated Heat Transfer;ASME J. Turbomach.,1998
3. Jovanovic, M. B., de Lange, H. C., and van Steenhoven, A. A., 2005, “Influence of Laser Drilling Imperfection on Film Cooling Performances,” ASME Paper No. GT2005-68251.10.1115/GT2005-68251
4. Demling, P., and Bogard, D. G., 2006, “The Effects of Obstructions on Film Cooling Effectiveness on the Suction Side of a Gas Turbine Vane,” ASME Paper No. GT2006-90577.10.115/GT2006-90577
5. Effects of Surface Deposition, Hole Blockage, and Thermal Barrier Coating Spallation on Vane Endwall Film Cooling;ASME J. Turbomach.,2007
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