A Detailed Uncertainty Analysis of Adiabatic Film Cooling Effectiveness Measurements Using Pressure-Sensitive Paint
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, FL 32816 e-mail:
2. GE Global Research, Niskayuna, NY 12309 e-mail:
3. GE Aviation, Lynn, MA 01905 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4032674/6304316/turbo_138_08_081007.pdf
Reference26 articles.
1. Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy;ASME J. Heat Transfer,1977
2. The Effectiveness of the Uniform Density, Two-Dimensional Wall Jet;Int. J. Heat Mass Transfer,1967
3. Film Cooling Downstream of a Row of Discrete Holes With Compound Angle,2001
4. Flate Plate Film Cooling Measurement Using PSP and Gas Chromatograph Techniques,1999
5. Theory for the Use of Foreign Gas in Simulating Film Cooling;Int. J. Heat Fluid Flow,1999
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