14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) 2008
DOI: 10.2514/6.2008-2887
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Cross-correlations of far field azimuthal modes in subsonic jet noise

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Cited by 16 publications
(19 citation statements)
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“…At the same time, there are also grounds to disregard the correlation of fields ξ n with different n for nonlinear turbulence pulsations. This follows from the experimental results in [12], which demonstrate an insignificant mutual correlation between the different azimuthal harmonics of acoustic far field radiation. Based on LES calculation for a turbulent jet, it was shown in [3] that the cross correlation coefficients of the Reynolds stress tensor components are character ized by relatively low values.…”
Section: Acoustic Radiation By a Random Field Of Quadrupole Sourcessupporting
confidence: 64%
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“…At the same time, there are also grounds to disregard the correlation of fields ξ n with different n for nonlinear turbulence pulsations. This follows from the experimental results in [12], which demonstrate an insignificant mutual correlation between the different azimuthal harmonics of acoustic far field radiation. Based on LES calculation for a turbulent jet, it was shown in [3] that the cross correlation coefficients of the Reynolds stress tensor components are character ized by relatively low values.…”
Section: Acoustic Radiation By a Random Field Of Quadrupole Sourcessupporting
confidence: 64%
“…the same time, similar to the approach based on monopole sources [1], such an approach is also incon sistent with experimental data [8,12], which indicate the quadrupole character of acoustic radiation. At first glance, the quadrupole character of acous tic radiation contradicts the fact that when the integral noise of the turbulent jet is measured by a single microphone (without preliminary harmonic decom position of a signal), sound radiation appears close to isotropic.…”
Section: Acoustic Radiation By a Random Field Of Quadrupole Sourcesmentioning
confidence: 71%
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“…In order to evaluate the possibility of measuring the noise of the turbulent jet in the anechoic chamber, the obtained measurement results had to be compared with the known results of similar tests in another anechoic chamber. For this purpose, it was used the results of measurements in anechoic chamber AC-2 TsAGI, which were performed for the jet rig with nozzle diameter D = 40 mm with a 6-microphones array of 0.85 m radius (figure 4) within the investigation of the azimuthal decomposition of turbulent jet noise [8]. From the data set, the points with coordinates θ = 30°, R = 1.7 m and θ = 90°, R = 0.85 m were taken.…”
Section: Measurements Of the Jet Noisementioning
confidence: 99%