Upstream nozzle shaping effects on near field flow in round turbulent free jets

https://doi.org/10.1016/j.euromechflu.2005.10.002Get rights and content

Abstract

Isothermal, incompressible round turbulent free jets of air, issuing from a sharp-edged orifice and from a contoured nozzle into still air surroundings, have been used to study the effects of upstream nozzle shaping on near field jet evolution experimentally. The Reynolds number, based on the diameter of the orifice or the nozzle, was 1.84×105 in both jets. Hot-wire anemometry and a pitot-static tube were used to obtain the measured quantities which included the mean streamwise velocity, the turbulent Reynolds normal and shear stresses, the autocorrelation coefficients and one-dimensional energy spectra of the fluctuating streamwise velocity and the mean static pressure. The mean streamwise velocity decay on the jet centerline and the jet half-velocity widths were obtained from the mean streamwise velocity data. To the extent that the results showed that mixing in the sharp-edged orifice round jet was higher than in the contoured nozzle round jet, upstream nozzle shaping was found to affect jet evolution in the near flow field. The distribution of the autocorrelation coefficients of the streamwise fluctuating velocity showed a marked difference in the evolution of the two jets, one of which had a uniform, and the other a non-uniform, exit plane mean streamwise velocity profile. The one-dimensional energy spectra results and also those of the distribution of the autocorrelation coefficients indicated the presence of coherent structures in the near field of the jets and the sharp-edged orifice jet was found to be more “energetic” than the contoured nozzle jet.

References (22)

  • W.R. Quinn et al.

    Effects of nonparallel exit flow on round turbulent free jets

    Int. J. Heat Fluid Flow

    (1989)
  • I. Wygnanski et al.

    Some measurements in the self-preserving jet

    J. Fluid Mech.

    (1969)
  • W. Rodi

    A new method of analyzing hot-wire signals in highly turbulent flow, and its evaluation in a round jet

    DISA Info

    (1975)
  • N.R. Panchapasekan et al.

    Turbulence measurements in axisymmetric jets of air and helium. Part 1: Air Jet

    J. Fluid Mech.

    (1993)
  • N. Rajaratnam

    Turbulent Jets

    (1976)
  • H. Schlichting

    Boundary-Layer Theory

    (1968)
  • S. Sami et al.

    Jet diffusion in the region of flow establishment

    J. Fluid Mech.

    (1967)
  • B.J. Hill

    Measurement of local entrainment rate in the initial region of axisymmetric turbulent air jets

    J. Fluid Mech.

    (1972)
  • L. Boguslawski et al.

    Flow structure of the free round turbulent jet in the initial region

    J. Fluid Mech.

    (1979)
  • N.T. Obot et al.

    The near field behaviour of round jets at moderate Reynolds numbers

    Canad. J. Chem. Engrg.

    (1984)
  • J. Mi et al.

    Mixing characteristics of axisymmetric free jets from a contoured nozzle, an orifice plate and a pipe

    J. Fluids Engrg.

    (2001)
  • Cited by (144)

    • Ignition of supercritical hydrothermal flames in co-flow jets

      2022, Journal of Supercritical Fluids
      Citation Excerpt :

      It has been reported that the length of the initial region for the round free turbulent jet can be determined by the product of an attenuation coefficient and nozzle diameter [43,44]. The attenuation coefficient generally varied in the range of 6–7, which depended on several factors, including the turbulence intensity of jet, the geometric structure of nozzle, and the amount of inflow entrainment near jet exit [45–47]. However, the calculated lengths of the jet initial region were about 5 times the nozzle diameter.

    View all citing articles on Scopus
    View full text