Scaling Considerations for Thermal and Pressure-Sensitive Paint Methods Used to Determine Adiabatic Effectiveness
Author:
Affiliation:
1. Air Force Research Laboratory, Wright-Patterson AFB, Fairborn, OH 45433
2. Air Force Institute of Technology, Wright-Patterson AFB, Fairborn, OH 45324
3. Air Force Institute of Technology, Wright-Patterson AFB, Fairborn, OH 45433
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4049102/6610925/turbo_143_1_011004.pdf
Reference17 articles.
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3. Turbine Blade Film Cooling Using PSP Technique;Han;Front. Heat Mass Transfer,2010
4. Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio;Sinha;ASME J. Turbomach.,1991
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