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Keywords: transonic
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Proceedings Papers

Proc. ASME. GT2022, Volume 6A: Heat Transfer — Combustors; Film Cooling, V06AT12A005, June 13–17, 2022
Paper No: GT2022-78519
...Proceedings of ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition GT2022 June 13-17, 2022, Rotterdam, The Netherlands GT2022-78519 OPTIMIZED FILM COOLING FLOW ON A CONTOURED ENDWALL WITHIN A TRANSONIC ANNULAR CASCADE Timothy A. Burdett, Izhar Ullah, Lesley M. Wright, and Je...
Proceedings Papers

Proc. ASME. GT2022, Volume 6A: Heat Transfer — Combustors; Film Cooling, V06AT12A040, June 13–17, 2022
Paper No: GT2022-83169
...Proceedings of ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition GT2022 June 13-17, 2022, Rotterdam, The Netherlands GT2022-83169 INTERACTION MECHANISM OF TRANSONIC SQUEALER TIP COOLING WITH THE EFFECT OF HIGH-SPEED RELATIVE CASING MOTION Wenbo Xie1, Hongmei Jiang1, Shaopeng...
Topics: Cooling
Proceedings Papers

Proc. ASME. GT2021, Volume 5A: Heat Transfer — Combustors; Film Cooling, V05AT12A015, June 7–11, 2021
Paper No: GT2021-59366
... the design process. blade tip film cooling transonic blowing ratio density ratio PSP technique blade tip flow leakage Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-59366 INFLUENCE OF COOLANT DENSITY...
Proceedings Papers

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A002, June 7–11, 2021
Paper No: GT2021-01771
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-01771 DEVELOPMENT OF LOSS CORRELATION AND TOOL VALIDATION AT TRANSONIC CONDITION BASED ON CASCADE TEST Jaewoo Choi1, David Simurda2, Jaewook Song1, Martin Luxa2...
Proceedings Papers

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A020, June 7–11, 2021
Paper No: GT2021-58828
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-58828 OVERVIEW OF UNSTEADY PHENOMENA EMERGING IN A STALLED 1.5-STAGE TRANSONIC COMPRESSOR Silas Mütschard Christoph Biela Jan Werner Sebastian Robens SIEMENS...
Topics: Compressors
Proceedings Papers

Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 255-270, June 14–18, 2010
Paper No: GT2010-22700
... to the experimental results. The test turbine was the unshrouded MT1 turbine, installed in the Turbine Test Facility (previously called Isentropic Light Piston Facility) at QinetiQ, Farnborough UK. This is a short duration transonic facility, which simulates engine representative M , Re, Tu, N / T and T...
Proceedings Papers

Proc. ASME. GT2007, Volume 6: Turbo Expo 2007, Parts A and B, 879-893, May 14–17, 2007
Paper No: GT2007-28123
...° relative to design incidence. MISES boundary layer method 2-D cascade validation transonic off-design HPT incidence loss CFD Proceedings of GT2007 ASME Turbo Expo 2007: Power for Land, Sea and Air May 14-17, 2007, Montreal, Canada Copyright © 2007 by ASME 1 cascade, validation, transonic...
Proceedings Papers

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 569-578, June 3–6, 2002
Paper No: GT2002-30383
..., such as -variant distortion. words: transonic, compressor, cfd, shock loss RODUCTION In general, the application of streamline curvature (SLC) hods to transonic fans has been limited. The SLC oaches do not typically include accurate fundamentally d off-design loss and deviation models (Bloch, et al., 6...
Proceedings Papers

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 803-811, June 3–6, 2002
Paper No: GT2002-30444
... a single-stage, isolated rotor the basis for experimental comparisons. Improved ance prediction is shown. The importance of properly ng for shock geometry and loss changes with operating ns is demonstrated. s: transonic, compressor, slc, loss, deviation UCTION urate and robust turbomachinery off-design...
Proceedings Papers

Proc. ASME. GT2003, Volume 6: Turbo Expo 2003, Parts A and B, 125-135, June 16–19, 2003
Paper No: GT2003-38079
.... The front-loaded generally inferior performance compared with foil. bine Aerodynamics, Transonic, Loading Limits arch Assistant. C Blade chord length Cb Base pressure coefficient, ( = (Pb P2)q2 ) Cx Axial chord length DFAC Diffusion FACtor d Leading edge diameter H Blade span i Incidence M Mach number o...
Proceedings Papers

Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 1015-1026, June 14–17, 2004
Paper No: GT2004-53087
... AND NUMERICAL INVE A FAMILY OF THREE HP TRA D. Corriveau Defence R&D Canada (DRDC-Valcartier) Quebec City, Quebec CANADA Email: Daniel.Corriveau@drdc-rddc.gc.ca ABSTRACT Experimental results concerning the performance of three high-pressure (HP) transonic turbine blades having fore-, aft- and mid-loadings have...
Proceedings Papers

Proc. ASME. GT2005, Volume 6: Turbo Expo 2005, Parts A and B, 451-464, June 6–9, 2005
Paper No: GT2005-68159
... 19 11 2008 Linear cascade measurements for the aerodynamic performance of three transonic High Pressure (HP) turbine blades have been presented previously by Corriveau and Sjolander [1] [2] for the design incidence. The airfoils were designed for the same inlet and outlet velocity...
Proceedings Papers

Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 809-820, May 8–11, 2006
Paper No: GT2006-90849
... 15 09 2008 Linear cascade measurements for the aerodynamic performance of a family of three transonic, high-pressure (HP) turbine blades have been presented previously by the authors. The airfoils were designed for the same inlet and outlet velocity triangles but varied...