Nonlinear interaction model of subsonic jet noise

• Published in: Philosophical transactions of the Royal Society of London. Series A: Mathematical, physical, and engineering sciences Vol. 366; no. 1876; pp. 2745 - 2760
• Main Authors: Sandham, Neil D, Salgado, Adriana M
• Format: Journal Article
• Language: English
• Published: London The Royal Society 13.08.2008
• Subjects: Acoustic instability; Aeroacoustics; Audio frequencies; Boundary conditions; Jet aircraft noise; Jet Noise; Mach number; Model airplanes; Parabolized Stability Equations; Strouhal numbers; Velocity distribution; Wave equations; Waves
• ISSN: 1364-503X; 1471-2962
• DOI: 10.1098/rsta.2008.0049

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.