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Keywords: Gas turbine blade cooling
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Proceedings Papers
Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A001, June 7–11, 2021
Publisher: American Society of Mechanical Engineers
Paper No: GT2021-58386
...-significant. gas turbine blade cooling conjugate heat transfer ribbed channel steam cooling Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-58386 STUDY ON CONJUGATE THERMAL PERFORMANCE OF A STEAM-COOLED RIBBED...
Proceedings Papers
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 67-79, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-22238
.... The effects of wall heat flux and mist ratio on mist cooling performance are also investigated in this study. 11 01 2011 Impinging jets mist cooling heat transfer enhancement multiphase flow gas turbine blade cooling curved surface Copyright © 2010 by ASME 1 Proceedings of GT2010 ASME...
Proceedings Papers
Proc. ASME. GT2009, Volume 3: Heat Transfer, Parts A and B, 149-159, June 8–12, 2009
Publisher: American Society of Mechanical Engineers
Paper No: GT2009-59282
... tested the case of one edge open exit configuration with single row of staggered effusion holes (Case-C1s) shows higher heat transfer among others. 23 02 2010 Gas turbine blade cooling Impingement cooling Film holes CFD Proceedings of ASME Turbo Expo 2009: Power for Land, Sea...
Proceedings Papers
Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 703-716, June 9–13, 2008
Publisher: American Society of Mechanical Engineers
Paper No: GT2008-50737
... transfer enhancement two-phase flow gas turbine blade cooling ( f p r b b c o t n u s c c r p a Proceedings of ASME Turbo Expo 2008: Power for Land, Sea and Air GT2008 June 9-13, 2008, Berlin, Germany Copyright © 2008 by ASME 1 all functions. In addition, the effect of different forces e.g. drag...
Proceedings Papers
Proc. ASME. GT2007, Volume 3: Turbo Expo 2007, 811-819, May 14–17, 2007
Publisher: American Society of Mechanical Engineers
Paper No: GT2007-28298
... cooling models from the actual (reported) corresponding values, was analyzed. It was found that for all three above blade cooling models the deviation was less than three percent for various classes of gas turbines. 10 03 2009 Gas Turbine Blade Cooling Gas Turbine Thermal Modeling...