1-5 of 5
Keywords: Reynolds number
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Proceedings Papers

Proc. ASME. GT2022, Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics, V10BT35A012, June 13–17, 2022
Paper No: GT2022-82426
... Abstract This paper presents the results of a numerical investigation on the influence of Reynolds number on the performance of a single stage centrifugal compressor with an outward wound volute with circular cross section. The main objectives of the presented work were to gain further...
Proceedings Papers

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A027, September 21–25, 2020
Paper No: GT2020-14672
...EFFECTS OF REYNOLDS NUMBER ON PERFORMANCE OF HIGHLY LOADED MULTI-STAGE AXIAL COMPRESSORS Xiaoshi Zhang AECC Commercial Aircraft Engine Co., Ltd, Shanghai, China ABSTRACT The influence of Reynolds number on performance of a highly loaded 10-stage axial compressor has been experimentally investigated...
Proceedings Papers

Proc. ASME. GT2020, Volume 7A: Heat Transfer, V07AT15A034, September 21–25, 2020
Paper No: GT2020-16115
...-channel models with different turning angles (45°, 60°, and 75°) and radiuses (0.6 mm, 0.9 mm, and 1.2 mm) were adopted to conduct the study, and the jet Reynolds number ranges from 10,000 to 40,000. The results show that the turning angle and turning internal radius affect the jet form significantly...
Proceedings Papers

Proc. ASME. GT2019, Volume 5A: Heat Transfer, V05AT11A005, June 17–21, 2019
Paper No: GT2019-90421
... Effects of Jetting Orifice Geometry Parameters and Channel Reynolds Number on Bended Channel Cooling for a Novel Internal Cooling Structure Wei He1, Qinghua Deng1,2 Juan He1, Tieyu Gao1, Zhenping Feng1 1. Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute...
Proceedings Papers

Proc. ASME. GT2003, Volume 1: Turbo Expo 2003, 317-328, June 16–19, 2003
Paper No: GT2003-38147
... 05 02 2009 The effects of Reynolds number on the non-nulling calibration of a typical cone-type five-hole probe have been investigated for the representative Reynolds numbers in turbomachinery. The pitch and yaw angles are changed from −35 degrees to 35 degrees with an angle interval...