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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
Paper No: GT2021-58386
.... temperature and temperature gradients of the blades to reduce the maximum thermal stress through efficient cooling Keywords: gas turbine blade cooling, conjugate heat technologies. Ribbed cooling channels have been widely used transfer, ribbed channel, steam cooling in the mid-chord region of turbine blades...
Proceedings Papers
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 67-79, June 14–18, 2010
Paper No: GT2010-22238
... of round jets. The effects of wall heat flux and mist ratio on mist cooling performance are also investigated in this study. 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
Paper No: GT2009-59282
... the configuration tested the case of one edge open exit configuration with single row of staggered effusion holes (Case-C1s) shows higher heat transfer among others. Gas turbine blade cooling Impingement cooling Film holes CFD Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air F S C ch...
Proceedings Papers
Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 703-716, June 9–13, 2008
Paper No: GT2008-50737
... 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, thermophoretic...
Proceedings Papers
Proc. ASME. GT2007, Volume 3: Turbo Expo 2007, 811-819, May 14–17, 2007
Paper No: GT2007-28298
... the above blade 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. Gas Turbine Blade Cooling Gas Turbine Thermal Modeling...
