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Simulation of impinging jet mass transfer at high Schmidt number with algebraic models

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Abstract
A simple method is proposed for simulation of impinging jet mass transfer at high Schmidt numbers. Two variants of algebraic models, based on the limiting behaviour of the turbulent diffusivity D(t) for y(+)-> 0, are employed in order to provide D(t) in the near-wall region while away from walls a formula based on the ratio of turbulent to molecular viscosity (v(t)/v) is applied for determination of the turbulent Schmidt number. Blending between the algebraic expressions and the formula for v(t)/v. is performed in the buffer region of the boundary layer, making the model independent of y(+) at larger distances from the walls. With the proposed models, very good results have been obtained for the mass transfer at high Schmidt number in impinging jet flows. The model also functions well at low Schmidt number.
Keywords
LARGE-EDDY SIMULATION, TURBULENT HEAT-TRANSFER, CHANNEL FLOW, SLOT-JET, PRANDTL NUMBER, TEMPERATURE-FIELDS, WALL, PLANE, PREDICTION, DIRECT NUMERICAL-SIMULATION, k-ω model, algebraic model, impinging jet flows, turbulence modelling, high-Schmidt mass transfer

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MLA
Kubacki, Slawomir, and Erik Dick. “Simulation of Impinging Jet Mass Transfer at High Schmidt Number with Algebraic Models.” PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, vol. 11, no. 1, 2011, pp. 30–41, doi:10.1504/PCFD.2011.037570.
APA
Kubacki, S., & Dick, E. (2011). Simulation of impinging jet mass transfer at high Schmidt number with algebraic models. PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 11(1), 30–41. https://doi.org/10.1504/PCFD.2011.037570
Chicago author-date
Kubacki, Slawomir, and Erik Dick. 2011. “Simulation of Impinging Jet Mass Transfer at High Schmidt Number with Algebraic Models.” PROGRESS IN COMPUTATIONAL FLUID DYNAMICS 11 (1): 30–41. https://doi.org/10.1504/PCFD.2011.037570.
Chicago author-date (all authors)
Kubacki, Slawomir, and Erik Dick. 2011. “Simulation of Impinging Jet Mass Transfer at High Schmidt Number with Algebraic Models.” PROGRESS IN COMPUTATIONAL FLUID DYNAMICS 11 (1): 30–41. doi:10.1504/PCFD.2011.037570.
Vancouver
1.
Kubacki S, Dick E. Simulation of impinging jet mass transfer at high Schmidt number with algebraic models. PROGRESS IN COMPUTATIONAL FLUID DYNAMICS. 2011;11(1):30–41.
IEEE
[1]
S. Kubacki and E. Dick, “Simulation of impinging jet mass transfer at high Schmidt number with algebraic models,” PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, vol. 11, no. 1, pp. 30–41, 2011.
@article{1908931,
  abstract     = {{A simple method is proposed for simulation of impinging jet mass transfer at high Schmidt numbers. Two variants of algebraic models, based on the limiting behaviour of the turbulent diffusivity D(t) for y(+)-> 0, are employed in order to provide D(t) in the near-wall region while away from walls a formula based on the ratio of turbulent to molecular viscosity (v(t)/v) is applied for determination of the turbulent Schmidt number. Blending between the algebraic expressions and the formula for v(t)/v. is performed in the buffer region of the boundary layer, making the model independent of y(+) at larger distances from the walls. With the proposed models, very good results have been obtained for the mass transfer at high Schmidt number in impinging jet flows. The model also functions well at low Schmidt number.}},
  author       = {{Kubacki, Slawomir and Dick, Erik}},
  issn         = {{1468-4349}},
  journal      = {{PROGRESS IN COMPUTATIONAL FLUID DYNAMICS}},
  keywords     = {{LARGE-EDDY SIMULATION,TURBULENT HEAT-TRANSFER,CHANNEL FLOW,SLOT-JET,PRANDTL NUMBER,TEMPERATURE-FIELDS,WALL,PLANE,PREDICTION,DIRECT NUMERICAL-SIMULATION,k-ω model,algebraic model,impinging jet flows,turbulence modelling,high-Schmidt mass transfer}},
  language     = {{eng}},
  number       = {{1}},
  pages        = {{30--41}},
  title        = {{Simulation of impinging jet mass transfer at high Schmidt number with algebraic models}},
  url          = {{http://doi.org/10.1504/PCFD.2011.037570}},
  volume       = {{11}},
  year         = {{2011}},
}

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