The intrinsic structure of turbulent jets

Lau, J. C.; Fisher, Michael J.; Fuchs, Helmut V.

doi:10.1016/0022-460x(72)90451-8

Cited by 125 publications

(60 citation statements)

References 6 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…This phase opposition for the streamwise velocity is found in coherent, axisymmetric vortical structures obtained by phase averages of forced jets (Hussain & Zaman 1981;Cohen & Wygnanski 1987;Petersen & Samet 1988), and was also seen previously in unforced jets by Lau, Fisher & Fuchs (1972). An illustration of such structures is shown in figure 18(b).…”

Section: Cross-stream Planessupporting

confidence: 80%

Wavepackets in the velocity field of turbulent jets

et al. 2013

View full text Add to dashboard Cite

We study the velocity fields of unforced, high Reynolds number, subsonic jets, issuing from round nozzles with turbulent boundary layers. The objective of the study is to educe wavepackets in such flows and to explore their relationship with the radiated sound. The velocity field is measured using a hot-wire anemometer and a stereoscopic, time-resolved PIV system. The field can be decomposed into frequency and azimuthal Fourier modes. The low-angle sound radiation is measured synchronously with a microphone ring array. Consistent with previous observations, the azimuthal wavenumber spectra of the velocity and acoustic pressure fields are distinct. The velocity spectrum of the initial mixing layer exhibits a peak at azimuthal wavenumbers m ranging from 4 to 11, and the peak is found to scale with the local momentum thickness of the mixing layer. The acoustic pressure field is, on the other hand, predominantly axisymmetric, suggesting an increased relative acoustic efficiency of the axisymmetric mode of the velocity field, a characteristic that can be shown theoretically to be caused by the radial compactness of the sound source. This is confirmed by significant correlations, as high as 10 %, between the axisymmetric modes of the velocity and acoustic pressure fields, these values being significantly higher than those reported for two-point flow-acoustic correlations in subsonic jets. The axisymmetric and first helical modes of the velocity field are then compared with solutions of linear parabolized stability equations (PSE) to ascertain if these modes correspond to linear wavepackets. For all but the lowest frequencies close agreement is obtained for the spatial amplification, up to the end of the potential core. The radial shapes of the linear PSE solutions also agree with the experimental results over the same region. The results suggests that, despite the broadband character of the turbulence, the evolution of Strouhal numbers 0.3 St 0.9 and azimuthal modes 0 and 1 can be modelled as linear wavepackets, and these are associated with the sound radiated to low polar angles.

show abstract

Section: Cross-stream Planessupporting

confidence: 80%

Wavepackets in the velocity field of turbulent jets

et al. 2013

View full text Add to dashboard Cite

show abstract

“…This low amplitude is seen in figure 21(b) to correspond to a position where the phase has an jump of π. The two sides of the jet mixing layer present a phase opposition for the axial velocity, a feature observed in forced jets (Cohen & Wygnanski 1987;Petersen & Samet 1988), but also in natural, turbulent jets (Lau, Fisher & Fuchs 1972). The source defined in (5.2) was used in (5.1) to obtain the radiated sound field for azimuthal modes 0, 1 and 2 as…”

Section: Sound Radiation By Helical Wavepacketsmentioning

confidence: 99%

Axisymmetric superdirectivity in subsonic jets

et al. 2012

View full text Add to dashboard Cite

We present experimental results for the acoustic field of jets with Mach numbers between 0.35 and 0.6. An azimuthal ring array of six microphones, whose polar angle, θ , was progressively varied, allows the decomposition of the acoustic pressure into azimuthal Fourier modes. In agreement with past observations, the sound field for low polar angles (measured with respect to the jet axis) is found to be dominated by the axisymmetric mode, particularly at the peak Strouhal number. The axisymmetric mode of the acoustic field can be clearly associated with an axially non-compact source, in the form of a wavepacket: the sound pressure level for peak frequencies is found be superdirective for all Mach numbers considered, with exponential decay as a function of (1 − M c cos θ ) 2 , where M c is the Mach number based on the phase velocity U c of the convected wave. While the mode m = 1 spectrum scales with Strouhal number, suggesting that its energy content is associated with turbulence scales, the axisymmetric mode scales with Helmholtz number -the ratio between source length scale and acoustic wavelength. The axisymmetric radiation has a stronger velocity dependence than the higher-order azimuthal modes, again in agreement with predictions of wavepacket models. We estimate the axial extent of the source of the axisymmetric component of the sound field to be of the order of six to eight jet diameters. This estimate is obtained in two different ways, using, respectively, the directivity shape and the velocity exponent of the sound radiation. The analysis furthermore shows that compressibility plays a significant role in the wavepacket dynamics, even at this low Mach number. Velocity fluctuations on the jet centreline are reduced as the Mach number is increased, an effect that must be accounted for in order to obtain a correct estimation of the velocity dependence of sound radiation. Finally, the higher-order azimuthal modes of the sound field are considered, and a model for the low-angle sound radiation by helical wavepackets is developed. The measured sound for azimuthal modes 1 and 2 at low Strouhal numbers is seen to correspond closely to the predicted directivity shapes.

show abstract

“…The flow characteristics of a circular jet have been extensively studied with emphasis on large-scale vortex structures; for example, periodic vortex rings were investigated using flow visualization [3], velocity and pressure fluctuation spectra [4], and vorticity distribution [5]. At moderate Reynolds numbers, vortex formation occurs due to Kelvin-Helmholtz instability in the region closest to the jet nozzle exit.…”

Section: Introductionmentioning

confidence: 99%