COMPUTATIONAL AEROACOUSTICS EXAMPLES SHOWING THE FAILURE OF THE ACOUSTIC ANALOGY THEORY TO IDENTIFY THE CORRECT NOISE SOURCES

DOI10.1142/S0218396X02001607zbMath1360.76302OpenAlexW2068892892MaRDI QIDQ2981720

Christopher K. W. Tam

Publication date: 9 May 2017

Published in: Journal of Computational Acoustics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0218396x02001607

zbMATH Keywords

computational aeroacousticsacoustic analogynoise source identififcation

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05)

Related Items (3)

A coupled time-reversal/complex differentiation method for aeroacoustic sensitivity analysis: towards a source detection procedure ⋮ Extensions of Lighthill's acoustic analogy with application to computational aeroacoustics ⋮ Quadratic stochastic estimation of far-field acoustic pressure with coherent structure events in a 2D compressible plane mixing layer

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• Direct computation of the sound generated by vortex pairing in an axisymmetric jet
• Sound generation in a mixing layer
• Computation of jet mixing noise due to coherent structures: the plane jet case
• Use of Linearized Euler Equations for Supersonic Jet Noise Prediction
• Direct computation of the sound from a compressible co-rotating vortex pair
• Sound generation by turbulence and surfaces in arbitrary motion
• Directional acoustic radiation from a supersonic jet generated by shear layer instability
• On sound generated aerodynamically I. General theory
• On sound generated aerodynamically II. Turbulence as a source of sound

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