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Keywords: Cross-flow
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Proceedings Papers

Proc. ASME. GT2020, Volume 7A: Heat Transfer, V07AT11A007, September 21–25, 2020
Paper No: GT2020-15139
...EXPERIMENTAL STUDY ON HEAT TRANSFER CHARACTERISTICS OF ARRAY IMPINGEMENT WITH INITIAL CROSS-FLOW Tian-liang Zhou1, Wei-jiang Xu1 2, Xiao-yu Shi1, Bo Su1, Fei Lu1 1 School of Power and Energy, Northwestern Polytechnical University, Shaanxi, Xi an, China 2 Shaanxi Key Laboratory of Thermal Sciences...
Proceedings Papers

Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A011, September 21–25, 2020
Paper No: GT2020-14389
... EXPERIMENTAL AND NUMERICAL STUDY ON THE EFFECTS OF THE RELATIVE POSITION OF FILM HOLE AND ORIENTATION RIBS ON THE FILM COOLING WITH RIBBED CROSS-FLOW COOLANT CHANNEL Bingran Li1, Cunliang Liu1,2, Lin Ye1, Huiren Zhu1,2, Fan Zhang1 1School of Power and Energy, Northwestern Polytechnical University...
Proceedings Papers

Proc. ASME. GT2012, Volume 4: Heat Transfer, Parts A and B, 1899-1912, June 11–15, 2012
Paper No: GT2012-68209
... by a screw compressor and can be regulated independently to supply the inner and outer an- nular passages of the test rig. It allows measurements of the discharge coefficient with cross flow and co- and counter-rotating shafts with cen- trifugal and centripetal flow through the rotating holes. On the outer...
Proceedings Papers

Proc. ASME. GT2012, Volume 4: Heat Transfer, Parts A and B, 1373-1380, June 11–15, 2012
Paper No: GT2012-68560
... S-bend diffuser pressure recovery effusion cooling cross-flow The experimental study considered passive effusion cooling in an S-bend diffusing passage in which ambient cool air was drawn naturally into the S-duct passage with sub-atmospheric flow distributions. Seven-hole pressure...
Proceedings Papers

Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 1051-1060, June 14–18, 2010
Paper No: GT2010-22691
..., with cross-flow included and on parameters suitable for correlation of the test data. A test rig was designed to simulate shaft diameters, rotation speeds and pressure ratios typical for real gas turbine designs. The pressure ratio across the orifices varied from 1.05 to 1.5 and the Mach number of the flow...
Proceedings Papers

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 1599-1612, June 9–13, 2008
Paper No: GT2008-50976
.... The influence of different geometric features is incorporated into a model for the calculation of discharge coefficients. Cross-flow discharge coefficient rotating orifice secondary air system SM NT C AL ü e A hu In an effort to provide usable further insight into flows Reax Axial Reynolds number...