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Philos Trans A Math Phys Eng Sci. 2008 Aug 13;366(1876):2745-60. doi: 10.1098/rsta.2008.0049.

Nonlinear interaction model of subsonic jet noise.

Author information

1
Aerodynamics and Flight Mechanics, School of Engineering Sciences, University of Southampton, Southampton SO17 1BJ, UK. n.sandham@soton.ac.uk

Abstract

Noise generation in a subsonic round jet is studied by a simplified model, in which nonlinear interactions of spatially evolving instability modes lead to the radiation of sound. The spatial mode evolution is computed using linear parabolized stability equations. Nonlinear interactions are found on a mode-by-mode basis and the sound radiation characteristics are determined by solution of the Lilley-Goldstein equation. Since mode interactions are computed explicitly, it is possible to find their relative importance for sound radiation. The method is applied to a single stream jet for which experimental data are available. The model gives Strouhal numbers of 0.45 for the most amplified waves in the jet and 0.19 for the dominant sound radiation. While in near field axisymmetric and the first azimuthal modes are both important, far-field sound is predominantly axisymmetric. These results are in close correspondence with experiment, suggesting that the simplified model is capturing at least some of the important mechanisms of subsonic jet noise.

PMID:
18487126
DOI:
10.1098/rsta.2008.0049

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