Unsteady Analysis of Blade and Tip Heat Transfer as Influenced by the Upstream Momentum and Thermal Wakes
Author:
Affiliation:
1. Department of Aerospace Engineering, Ohio State University, Columbus, OH 43210
2. ASRC Aerospace, NASA Glenn Research Center, Cleveland, OH 44135
3. A and E Consulting, Westlake, OH 44140
4. NASA Glenn Research Center, Cleveland, OH 44135
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.3213549/5844703/041007_1.pdf
Reference20 articles.
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3. Unsteady Heat Transfer in Stator-Rotor Interaction by Two-Equation Turbulence Mode;Michelassi;ASME J. Turbomach.
4. Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations;Abhari;ASME J. Turbomach.
5. Ameri, A. A., Rigby, D., Heidmann, J., Steinthorsson, E., and Fabian, J., 2006, “Effects of Unsteadiness Due to Wake Passing on Rotor Blade Heat Transfer,” AIAA Paper No. AIAA-2006-3263.
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