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1-8 of 8
Keywords: turbine blade cooling
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Proceedings Papers
Proc. ASME. GT2022, Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling, V06BT15A024, June 13–17, 2022
Paper No: GT2022-82797
... rotating heat transfer serpentine channel bleed holes mass flow rate ratio turbine blade cooling Abstract The effect of rotation on heat transfer in a typical turbine blade middle-chord channel is experimentally investigated. The channel is characterized by ribs, three-pass serpentine...
Proceedings Papers
Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A022, June 7–11, 2021
Paper No: GT2021-60182
... turbine blade cooling two-pass channel cross bridge dimple rotation heat transfer Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-60182 ROTATING COOLING PERFORMANCE OF TWO-PASS RECTANGULAR CHANNELS...
Proceedings Papers
Proc. ASME. GT2013, Volume 3A: Heat Transfer, V03AT12A043, June 3–7, 2013
Paper No: GT2013-95445
... cooling performance, as much as 50% higher than the conventional configuration. Turbine blade cooling Internal passage Trailing edge Perforated blockages Naphthalene sublimation 1 Copyright © 2013 by ASME TRAILING EDGE COOLING OF A GAS TURBINE BLADE WITH PERFORATED BLOCKAGES WITH INCLINED...
Proceedings Papers
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 555-567, June 14–18, 2010
Paper No: GT2010-23510
... the heater glass in order to provide transparent models. Turbine Blade Cooling Two-Pass System Ribs Bend U-Turn Flow Turning Dean Vortex Separation Rotation Flow Measurement Particle Image Velocimetry PIV 1 Copyright © 2010 by ASME Proceedings of ASME TURBO EXPO 2010 June 14-18, 2010...
Proceedings Papers
Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 1039-1050, June 9–13, 2008
Paper No: GT2008-51183
... for the development and validation of numerical simulation tools like the DLR flow solver TRACE which is not a topic of this paper. Turbine Blade Cooling Two-Pass System Ribs Bend U-Turn Flow Turning Dean Vortex Separation Rotation Flow Measurement Particle Image Velocimetry PIV Laser Optic...
Proceedings Papers
Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 533-545, June 14–17, 2004
Paper No: GT2004-53566
... PIV, respectively. Turbine Blade Cooling Two-Pass System Ribs 180deg. Bend U-Turn Dean Vortex Separation Flow Field Measurement Laser Techniques L2F PIV Visualization Proceedings of ASME TURBO EXPO 2004 June 14-17, 2004, Vienna, Austria Proceedings of ASME Turbo Expo 2004 Power...
Proceedings Papers
Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 943-950, June 14–17, 2004
Paper No: GT2004-54206
... achieve more than 100% within 2 jet-diameter distance from the stagnation line at Re = 15,000 and m l /m s = 1.5%. jets impingement mist/steam heat transfer turbine blade cooling future of high-temperature gas turbine systems that burn hydrogen or synthe heat t chann gener pressu distan rows...
Proceedings Papers
Proc. ASME. GT2005, Volume 3: Turbo Expo 2005, Parts A and B, 919-929, June 6–9, 2005
Paper No: GT2005-69100
... is performed on the effect of flue gas temperature, blowing angle, blowing ratio, mist injection rate, and droplet size on the cooling effectiveness with 2-D cases. Analysis on droplet history (trajectory and size) is undertaken to interpret the mechanism of droplet dynamics. film cooling turbine blade...
