Unsteady Effects on the Experimental Determination of Overall Effectiveness
Author:
Affiliation:
1. Air Force Institute of Technology, Wright-Patterson Air Force Base, Air Force Base, OH 45433 e-mail:
2. Air Force Institute of Technology, Wright-Patterson Air Force Base, Air Force Base, OH 45433
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4041233/6309580/turbo_140_12_121005.pdf
Reference14 articles.
1. Sensitivity of the Overall Effectiveness to Film Cooling and Internal Cooling on a Turbine Vane Suction Side;ASME J. Turbomach.,2014
2. Albert, J. E., Bogard, D. G., and Cunha, F., 2004, “Adiabatic and Overall Effectiveness for a Film Cooled Blade,” ASME Paper No. GT2004-53998.10.1115/GT2004-53998
3. Determination of Cooling Parameters for a High Speed, True Scale, Metallic Turbine Vane;ASME J. Turbomach.,2017
4. Computational Fluid Dynamics Evaluations of Film Cooling Flow Scaling Between Engine and Experimental Conditions;ASME J. Turbomach.,2017
5. Impact of Rotor-Stator Interaction on Turbine Blade Film Cooling;ASME J. Turbomach.,1996
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