Crackle-related beamforming of military jet aircraft noise

Vaughn, Aaron B.; Gee, Kent L.; Swift, S. Hales; Wall, Alan T.; Downing, J. Micah; James, Michael M.

doi:10.2514/6.2019-2664

Cited by 2 publications

(1 citation statement)

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“…[61] stress that source nonlinearity does not mean that nonlinear propagation does not exacerbate the problem. Such effects complicate the inversion of near-field pressure signals back to their source and seem evident in recent analysis [62] of F-35 noise measurements. Further exploration of these problems combining simulations, test data and nonlinear propagation models is warranted.…”

Section: Large-eddy Simulations As a Complement To Experimentsmentioning

confidence: 99%

Modelling of jet noise: a perspective from large-eddy simulations

Brès

Lele

2019

Phil. Trans. R. Soc. A.

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In the last decade, many research groups have reported predictions of jet noise using high-fidelity large-eddy simulations (LES) of the turbulent jet flow and these methods are beginning to be used more broadly. A brief overview of the publications since the review by Bodony & Lele (2008, AIAA J. 56 , 346–380) is undertaken to assess the progress and overall contributions of LES towards a better understanding of jet noise. In particular, we stress the meshing, numerical and modelling advances which enable detailed geometric representation of nozzle shape variations intended to impact the noise radiation, and sufficiently accurate capturing of the turbulent boundary layer at the nozzle exit. Examples of how LES is currently being used to complement experiments for challenging conditions (such as highly heated pressure-mismatched jets with afterburners) and guide jet modelling efforts are highlighted. Some of the physical insights gained from these numerical studies are discussed, in particular on crackle, screech and shock-associated noise, impingement tones, acoustic analogy models, wavepackets dynamics and resonant acoustic waves within the jet core. We close with some perspectives on the remaining challenges and upcoming opportunities for future applications. This article is part of the theme issue ‘Frontiers of aeroacoustics research: theory, computation and experiment’.

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Section: Large-eddy Simulations As a Complement To Experimentsmentioning

confidence: 99%