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Direct computation of perturbed impinging hot jets

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Direct computation of perturbed impinging hot jets. / Jiang, X.; Zhao, H.; Luo, K. H. et al.
In: Computers and Fluids, Vol. 36, No. 2, 02.2007, p. 259-272.

Research output: Contribution to Journal/MagazineJournal articlepeer-review

Harvard

Jiang, X, Zhao, H, Luo, KH & Jiang, X 2007, 'Direct computation of perturbed impinging hot jets', Computers and Fluids, vol. 36, no. 2, pp. 259-272. https://doi.org/10.1016/j.compfluid.2006.01.015

APA

Jiang, X., Zhao, H., Luo, K. H., & Jiang, X. (2007). Direct computation of perturbed impinging hot jets. Computers and Fluids, 36(2), 259-272. https://doi.org/10.1016/j.compfluid.2006.01.015

Vancouver

Jiang X, Zhao H, Luo KH, Jiang X. Direct computation of perturbed impinging hot jets. Computers and Fluids. 2007 Feb;36(2):259-272. doi: 10.1016/j.compfluid.2006.01.015

Author

Jiang, X. ; Zhao, H. ; Luo, K. H. et al. / Direct computation of perturbed impinging hot jets. In: Computers and Fluids. 2007 ; Vol. 36, No. 2. pp. 259-272.

Bibtex

@article{66e3eb035fa1465ea0f107b65ea37d99,
title = "Direct computation of perturbed impinging hot jets",
abstract = "The unsteady flow and temperature fields of an impinging hot jet at a Reynolds number of 1000 and a nozzle-to-plate distance of 6 jet diameters have been obtained by direct numerical solution of the compressible time-dependent three-dimensional Navier-Stokes equations using highly accurate numerical methods. Effects of an external perturbation on the flow and heat transfer characteristics of the transitional impinging jet have been examined. Oscillatory behaviour induced by the external perturbation has been observed for the impinging jet. The external perturbation leads to the large-scale vortical structures in the primary jet stream, which subsequently lead to the strong oscillatory behaviour of the impinging jet. The vortical structures lead to flow transitional behaviour that enhances mixing of the hot jet with the ambient fluid. It has been observed that the wall boundary layer of the impinging jet is thin. Both the instantaneous and time-averaged wall shear and normal stresses and Nusselt number are examined. Although the external perturbation strongly affects the flow structures in the primary jet stream, it does not have significant effects on the wall stresses and heat transfer characteristics of the impinging jet due to the re-laminarization effect of the wall. (c) 2006 Elsevier Ltd. All rights reserved.",
keywords = "DIRECT NUMERICAL-SIMULATION, LARGE-EDDY SIMULATIONS, IMPINGEMENT HEAT-TRANSFER, ACOUSTIC EXCITATION, BOUNDARY-CONDITIONS, TURBULENCE MODEL, FLOW, DYNAMICS, SCHEMES, FIELD",
author = "X. Jiang and H. Zhao and Luo, {K. H.} and Xi Jiang",
year = "2007",
month = feb,
doi = "10.1016/j.compfluid.2006.01.015",
language = "English",
volume = "36",
pages = "259--272",
journal = "Computers and Fluids",
issn = "0045-7930",
publisher = "Elsevier Limited",
number = "2",

}

RIS

TY - JOUR

T1 - Direct computation of perturbed impinging hot jets

AU - Jiang, X.

AU - Zhao, H.

AU - Luo, K. H.

AU - Jiang, Xi

PY - 2007/2

Y1 - 2007/2

N2 - The unsteady flow and temperature fields of an impinging hot jet at a Reynolds number of 1000 and a nozzle-to-plate distance of 6 jet diameters have been obtained by direct numerical solution of the compressible time-dependent three-dimensional Navier-Stokes equations using highly accurate numerical methods. Effects of an external perturbation on the flow and heat transfer characteristics of the transitional impinging jet have been examined. Oscillatory behaviour induced by the external perturbation has been observed for the impinging jet. The external perturbation leads to the large-scale vortical structures in the primary jet stream, which subsequently lead to the strong oscillatory behaviour of the impinging jet. The vortical structures lead to flow transitional behaviour that enhances mixing of the hot jet with the ambient fluid. It has been observed that the wall boundary layer of the impinging jet is thin. Both the instantaneous and time-averaged wall shear and normal stresses and Nusselt number are examined. Although the external perturbation strongly affects the flow structures in the primary jet stream, it does not have significant effects on the wall stresses and heat transfer characteristics of the impinging jet due to the re-laminarization effect of the wall. (c) 2006 Elsevier Ltd. All rights reserved.

AB - The unsteady flow and temperature fields of an impinging hot jet at a Reynolds number of 1000 and a nozzle-to-plate distance of 6 jet diameters have been obtained by direct numerical solution of the compressible time-dependent three-dimensional Navier-Stokes equations using highly accurate numerical methods. Effects of an external perturbation on the flow and heat transfer characteristics of the transitional impinging jet have been examined. Oscillatory behaviour induced by the external perturbation has been observed for the impinging jet. The external perturbation leads to the large-scale vortical structures in the primary jet stream, which subsequently lead to the strong oscillatory behaviour of the impinging jet. The vortical structures lead to flow transitional behaviour that enhances mixing of the hot jet with the ambient fluid. It has been observed that the wall boundary layer of the impinging jet is thin. Both the instantaneous and time-averaged wall shear and normal stresses and Nusselt number are examined. Although the external perturbation strongly affects the flow structures in the primary jet stream, it does not have significant effects on the wall stresses and heat transfer characteristics of the impinging jet due to the re-laminarization effect of the wall. (c) 2006 Elsevier Ltd. All rights reserved.

KW - DIRECT NUMERICAL-SIMULATION

KW - LARGE-EDDY SIMULATIONS

KW - IMPINGEMENT HEAT-TRANSFER

KW - ACOUSTIC EXCITATION

KW - BOUNDARY-CONDITIONS

KW - TURBULENCE MODEL

KW - FLOW

KW - DYNAMICS

KW - SCHEMES

KW - FIELD

U2 - 10.1016/j.compfluid.2006.01.015

DO - 10.1016/j.compfluid.2006.01.015

M3 - Journal article

VL - 36

SP - 259

EP - 272

JO - Computers and Fluids

JF - Computers and Fluids

SN - 0045-7930

IS - 2

ER -