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Film-Cooling Effectiveness From Shaped Film Cooling Holes for a Gas Turbine Blade
Volume 4: Heat Transfer, Parts A and B, 2008The effect of film cooling holes placed along the span of a fully-cooled high pressure turbine blade in a stationary, linear cascade on film cooling effectiveness is studied using the Pressure Sensitive Paint (PSP) technique. Six rows of compound angled shaped film cooling holes are provided on the pressure side while four such rows are provided on the
Shantanu Mhetras +2 more
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Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades
Journal of Engineering for Gas Turbines and Power, 1984Film cooling has become a standard method for the protection of the skin of gas turbine blades against the influence of the hot gas stream. The cooling air is usually injected into the boundary layer covering the skin through one or two rows of holes.
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Study on cooling efficiency of film cooling
The Proceedings of Conference of Chugoku-Shikoku Branch, 2019Kazuki Yamamoto +3 more
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A-to-Z Guide to Thermodynamics, Heat and Mass Transfer, and Fluids Engineering, 2006
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Recent advances in film cooling enhancement: A review
Chinese Journal of Aeronautics, 2020Jing-Zhou Zhang
exaly
Transpiration Cooling: Contribution of Film Cooling to the Overall Cooling Effectiveness
International Journal of Turbo and Jet Engines, 1986G.E. Andrews +3 more
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