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Keywords: turbine blade cooling
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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
... chord cooling technology for gas turbine blade. 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...
Proceedings Papers

Proc. ASME. GT2013, Volume 3A: Heat Transfer, V03AT12A043, June 3–7, 2013
Paper No: GT2013-95445
... Turbine blade cooling Internal passage Trailing edge Perforated blockages Naphthalene sublimation We propose an improved hole array to enhance the cooling performance of a perforated blockage. The internal passage in the trailing region of the blade was modeled as a wide square channel...
Proceedings Papers

Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 555-567, June 14–18, 2010
Paper No: GT2010-23510
... in order to provide transparent models. 11 01 2011 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...
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
..., respectively. 25 11 2008 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...
Proceedings Papers

Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 943-950, June 14–17, 2004
Paper No: GT2004-54206
...-diameter distance from the stagnation line at Re = 15,000 and m l /m s = 1.5%. 25 11 2008 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 The s condu...
Proceedings Papers

Proc. ASME. GT2005, Volume 3: Turbo Expo 2005, Parts A and B, 919-929, June 6–9, 2005
Paper No: GT2005-69100
... blade cooling mist cooling 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. Keywords: film cooling, turb Nomenclature b slot width (m) C concentration (kg/m cp specific heat (J...