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Keywords: thermal performance
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Journal Articles
Journal:
Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. November 2024, 146(11): 111006.
Paper No: TURBO-23-1085
Published Online: June 17, 2024
...S. W. Schekman; T. Kim The cooling configuration, sequentially combining perforated blockages (forming blockage jets) and a pin-fin array inside the trailing-edge of a turbine blade has been perceived unsuitable due to the presumed inferior thermal performance (η < 1.0). In the present study, we...
Journal Articles
Journal:
Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. November 2022, 144(11): 111006.
Paper No: TURBO-21-1234
Published Online: July 21, 2022
... size to channel height ratios considered G/H = 0.2, 0.3, and 0.4, respectively. The thermal performance of each fin configuration is determined from the measured pressure drop across the array and regionally averaged heat transfer coefficients at flow Reynolds numbers ranging Re = 20,000–80,000...
Journal Articles
Journal:
Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2011, 133(1): 011020.
Published Online: September 23, 2010
.... , 1999 , “ Effects of Hole Shape on Film Cooling With Large Angle Injection ,” ASME Paper No. 99-GT-165. Gritsch , M. , Colban , W. , and Schar , H. , 2005 , “ Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes ,” ASME J. Turbomach. 0889-504X , 127...