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CFD study of turbulent jet impingement on curved surface

CFD study of turbulent jet impingement on curved surface
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摘要 The heat transfer and flow characteristics of air jet impingement on a curved surface are investigated with computational fluid dynamics(CFD)approach.The first applied model is a one-equation SGS model for large eddy simulation(LES)and the second one is the SST-SAS hybrid RANS-LES.These models are utilized to study the flow physics in impinging process on a curved surface for different jet-to-surface(h/B)distances at two Reynolds numbers namely,2960 and 4740 based on the jet exit velocity(U_e)and the hydraulic diameter(2B).The predictions are compared with the experimental data in the literature and also the results from RANS k-εmodel.Comparisons show that both models can produce relatively good results.However,one-equation model(OEM)produced more accurate results especially at impingement region at lower jet-to-surface distances.In terms of heat transfer,the OEM also predicted better at different jet-to-surface spacings.It is also observed that both models show similar performance at higher h/B ratios. The heat transfer and flow characteristics of air jet impingement on a curved surface are investigated with com- putational fluid dynamics (CFD) approach. The first applied model is a one-equation SGS model for large eddy simulation (LES) and the second one is the SST-SAS hybrid RANS-LES, These models are utilized to study the flow physics in impinging process on a curved surface for different jet-to-surface (h/B) distances at two Reynolds numbers namely, 2960 and 4740 based on the jet exit velocity (Ue) and the hydraulic diameter (2B), The predic- tions are compared with the experimental data in the literature and also the results from RANS k-ε model. Com- parisons show that both models can produce relatively good results. However, one-equation model (OEM) produced more accurate results especially at impingement region at lower jet-to-surface distances. In terms of heat transfer, the OEM also predicted better at different jet-to-surface spacings. It is also observed that both models show similar performance at higher h/B ratios.
出处 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2016年第5期588-596,共9页 中国化学工程学报(英文版)
关键词 计算流体力学 射流冲击 曲面 原始设备制造商 方程模型 湍流 弯曲表面 射流特性 Jet impingement Curved surface RAST one-equation model Large eddy simulation Heat transfer
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  • 1M,A,R. Sharif, K.K. Mothe, Parametric study of turbulent slot-jet impingement heat transfer from concave cylindrical surfaces, lnt.J. Therm. Sci. 49 (2010) 428-442.
  • 2R.S. Amano, H. Brandt, Numerical study of turbulent axisymmetric jets impinging on a fiat plate and flowing into an axisymmetric cavity, ASMEJ. Fluids Eng. 106 (1984) 410-417.
  • 3D. Lytle, R.W. Webb, Air jet impingement heat transfer at low nozzle-to-plate spac- ings, Int.J. HeatMass Transfer37 (7) (1994) 1687-1697.
  • 4C. Cornaro, A.S. Fleischer, ILJ. Goldstein, Flow visualization of a round jet impinging on cylindrical surfaces, Exp. Therm. Fluid Sd. 20 (1999) 66-78.
  • 5S.D. Hwang, H.H. Cho, Effects of acoustic excitation positions on heat transfer and flow in axisymmetric impinging jet: main jet excitation and shear layer excitation, lnt..]. Heat Fluid Flaw 24 (1) (2003) 199-209.
  • 6L.A. EI-Gabray, D.A. Kaminski, Numerical investigation of jet impingement with cross flow: Comparison of Yang-Shih and standard k-turbulence model, Numer. Heat Transfer A 47 (2005) 441-469.
  • 7J.M. Miao, C.Y. Wu, P.H. Chert, Numerical investigation of confined multiple-jet im- pingement cooling over a flat plate at different crossflow orientations, Numer. Heat TransferA 55 (2009) 1019-1050.
  • 8H.Y. So, H.G. Yoon, M.K. Chung, Large eddy simulation of flow characteristics in an unconfined slot impinging jet with various nozzle-to-plate distances, Int. J. Mech. ScL Technol. 25 (3) (2011) 721-729.
  • 9J. Taghinia, M.M. Rahman, T. Siikonen, Numerical investigation of twin-jet impinge- ment with hybrid-type turbulence modeling, Appl. Therm. Eng. 73 (1) (2014) 648-657.
  • 10R.S. Bunker, D.E. Metzger, Local heat transfer in internally cooled turbine airfoil lead- ing edge regions. Part Ⅰ: Impingement cooling without film coolant extraction, J. Turhomach. 12 (1990) 451-458.

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