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Keywords: cutback
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Proceedings Papers

Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A043, September 21–25, 2020
Paper No: GT2020-15093
...BACKGROUND-GRID BASED MAPPING APPROACH TO FILM COOLING MESHING: PART II APPLICATIONS IN VANE WITH LANDED TRAILING-EDGE CUTBACK Ruiqin Wang, Xin Yan* Institute of Turbomachinery, Xi an Jiaotong University, Xi an 710049, China * Email: xinyan@mail.xjtu.edu.cn ABSTRACT As gas turbine inlet...
Proceedings Papers

Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A051, September 21–25, 2020
Paper No: GT2020-15346
...UNSTEADY NUMERICAL INVESTIGATION ON FILM COOLING CHARACTERISTICS OF THE TRAILING EDGE CUTBACK WITH UPSTREAM CYLINDER HOLE Xiangtao Xiao1,2, Pei Wang1,2, Qingzong Xu1,2, Qiang Du1,2, Jun Liu1,2, Sheng Chang1,2 1Key Lab of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese...
Proceedings Papers

Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A042, September 21–25, 2020
Paper No: GT2020-15092
... a considerable influence on film cooling performance in the cutback region. meshing film cooling full-cooled cutback land BACKGROUND-GRID BASED MAPPING APPROACH TO FILM COOLING MESHING: PART III APPLICATIONS IN A FULL-COOLED TURBINE VANE Ruiqin Wang, Xin Yan* Institute of Turbomachinery, Xi...
Proceedings Papers

Proc. ASME. GT2020, Volume 2E: Turbomachinery, V02ET41A035, September 21–25, 2020
Paper No: GT2020-15780
...VERY LARGE EDDY SIMULATION OF FILM COOLING EFFECTIVENESS ON TRAILING EDGE CUTBACK Xin Yan Institute of Turbomachinery, Xi an Jiaotong University, Xi an 710049, China Email: xinyan@mail.xjtu.edu.cn ABSTRACT The trailing edge of high pressure gas turbine blade in aero- engine is usually designed...