Noise generated by nearly axisymmetric vortex pairing in an excited low Mach number jet was studied experimentally as a prototypical jet noise source using a three-dimensional microphone array. The measured time-dependent sound field was decomposed into its multipole components using general linear regression techniques. Although the vortex interactions were very nearly axisymmetric and thus a nearly axisymmetric lateral quadrupole sound field was expected, the sound field was found to have large departures from axisymmetry. This acoustic sensitivity to symmetry breaking in the vorticity field was also shown in calculations using numerical vortex models and vortex sound theory. The directivity of the far-field sound gets smeared out in the time averaged data due to the tilting of the quadrupoles; this emphasizes the need for studying the jet sound pressure field in four dimensions (x, t) to better understand the mechanisms of noise generation.
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April 1995
Research Papers
Instantaneous Directivity in Jet Noise by Multipole Decomposition
A. Ghosh,
A. Ghosh
Department of Mechanical Engineering, University of Houston, Houston, TX
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J. Bridges,
J. Bridges
Department of Mechanical Engineering, University of Houston, Houston, TX
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F. Hussain
F. Hussain
Department of Mechanical Engineering, University of Houston, Houston, TX
Search for other works by this author on:
A. Ghosh
Department of Mechanical Engineering, University of Houston, Houston, TX
J. Bridges
Department of Mechanical Engineering, University of Houston, Houston, TX
F. Hussain
Department of Mechanical Engineering, University of Houston, Houston, TX
J. Vib. Acoust. Apr 1995, 117(2): 172-179 (8 pages)
Published Online: April 1, 1995
Article history
Received:
December 1, 1993
Online:
February 26, 2008
Citation
Ghosh, A., Bridges, J., and Hussain, F. (April 1, 1995). "Instantaneous Directivity in Jet Noise by Multipole Decomposition." ASME. J. Vib. Acoust. April 1995; 117(2): 172–179. https://doi.org/10.1115/1.2873876
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