- Acoustic analogy
Acoustic analogies are applied mostly in numerical aeroacoustics to reduce aeroacoustic sound sources to simple emitter types. They are therefore often also referred to as aeroacoustic analogies.
In general, aeroacoustic analogies are derived from the compressible
Navier-Stokes equations(NSE). The compressible NSE are rearranged into various forms of the inhomogeneous acoustic wave equation. Within these equations, source terms describe the acoustic sources. They consist of pressure and speed fluctuation as well as stress tensorand force terms. Approximationsare introduced to make the source terms independent of the acoustic variables. In this way, linearized equations are derive which describe the propagation of the acoustic waves in a homogeneous, resting medium. The latter is excited by the acoustic source terms, which are determined from the turbulent fluctuations. Since the aeroacoustics are described by the equations of classical acoustics, the methods are called aeroacoustic analogies.
The Lighthill-Analogy considers a free flow, as for example with an engine jet. The nonstationary fluctuations of the stream are represented by a distribution of
quadrupolesources in the same volume.
The Curle-Analogy is a formal solution of the Lighthill Analogy, which takes hard surfaces into consideration.
The Ffowcs Williams-Hawkings-Analogy is valid for aeroacoustic sources in relative motion with respect to a hard surface, as is the case in many technical applications for example in the automotive industry or in air travel. The calculation involves
quadrupole, dipoleand monopoleterms.
* Blumrich, R.: "Berechnungsmethoden für die Aeroakustik von Fahrzeugen". Tagungsband der ATZ/MTZ-Konferenz Akustik 2006, Stuttgart, 17-18.5.2006..
* Lighthill, M. J.: "On sound generated aerodynamically. I. General theory". Proc. Roy. Soc. 211(A) S. 564-587, London, 1952.
* Lighthill, M. J.: "On sound generated aerodynamically. I. General theory". Proc. Roy. Soc. 222(A) S. 1-34, London, 1954.
* Ffowcs Williams, J. E. and Hawkings, D. L.: "Sound Generation by Turbulence and Surfaces in Arbitrary Motion". Philosophical Transactions of the Royal Society, Vol. A264, Nr. 1151, 1969, S. 321-342
* Curle, N.: "The Influence of solid boundaries upon aerodynamic sound". Proc. Roy. Soc. Lond., A23, 505-514. 1955
* [http://www.ias.et.tu-dresden.de/akustik/Publikationen/Stroemungsakustik/koe2004_3.pdf Contribution of the Technical University of Dresden to the modeling of flow sound sources with elementary emitters.]
* [http://www.ias.et.tu-dresden.de/akustik/Publikationen/Stroemungsakustik/koe2000-1.pdf Contribution of the Technical University of Dresden to the history of aeroacoustics.]
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