Skip Nav Destination
1-3 of 3
Proc. ASME. GT2012, Volume 8: Turbomachinery, Parts A, B, and C, 1633-1645, June 11–15, 2012
Paper No: GT2012-69990
... is used for mesh generation and flow calculation. The results are presented comparing the pressure ratio and efficiency from numerical solutions and experimental data and flow properties distributions along the blade span. HPT CFD turbulence model O-grid structured mesh unstructured mesh 1...
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...
Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 277-286, June 14–17, 2004
Paper No: GT2004-54067
... thermodynamic investigations and detailed studies on optimised coolant injection geometries as well. HPT film cooling pressure side separated flow experimental and numerical results Proceedings of ASME Turbo Expo 2004 Power for Land, Sea and Air June 14-17, 2004, Vienna, Austria AERO-THERMODYNAMIC...