Theoretical and numerical method in aeroacoustics

The paper deals with the mathematical and numerical modeling of the aerodynamic noisegenerated by the fluid flow interaction with the solid structure of a rotor blade.Our analysis use Lighthill’s acoustic analogy. Lighthill idea was to express the fundamental equationsof motion into a wave equation...

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Main Authors: Nicuşor ALEXANDRESCU, Maria ALEXANDRESCU
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2010-06-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/maria_alexandrescu_v2no2_full.pdf
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author Nicuşor ALEXANDRESCU
Maria ALEXANDRESCU
author_facet Nicuşor ALEXANDRESCU
Maria ALEXANDRESCU
author_sort Nicuşor ALEXANDRESCU
collection DOAJ
description The paper deals with the mathematical and numerical modeling of the aerodynamic noisegenerated by the fluid flow interaction with the solid structure of a rotor blade.Our analysis use Lighthill’s acoustic analogy. Lighthill idea was to express the fundamental equationsof motion into a wave equation for acoustic fluctuation with a source term on the right-hand side. Theobtained wave equation is solved numerically by the spatial discretization. The method is applied inthe case of monopole source placed in different points of blade surfaces to find this effect of noisepropagation.
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spelling doaj.art-3a8ce0a908b84a9787622e791003b8542022-12-21T18:53:02ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282010-06-012231310.13111/2066-8201.2010.2.2.1Theoretical and numerical method in aeroacousticsNicuşor ALEXANDRESCUMaria ALEXANDRESCUThe paper deals with the mathematical and numerical modeling of the aerodynamic noisegenerated by the fluid flow interaction with the solid structure of a rotor blade.Our analysis use Lighthill’s acoustic analogy. Lighthill idea was to express the fundamental equationsof motion into a wave equation for acoustic fluctuation with a source term on the right-hand side. Theobtained wave equation is solved numerically by the spatial discretization. The method is applied inthe case of monopole source placed in different points of blade surfaces to find this effect of noisepropagation.http://bulletin.incas.ro/files/maria_alexandrescu_v2no2_full.pdfnoiseaero-acousticdiscretization
spellingShingle Nicuşor ALEXANDRESCU
Maria ALEXANDRESCU
Theoretical and numerical method in aeroacoustics
INCAS Bulletin
noise
aero-acoustic
discretization
title Theoretical and numerical method in aeroacoustics
title_full Theoretical and numerical method in aeroacoustics
title_fullStr Theoretical and numerical method in aeroacoustics
title_full_unstemmed Theoretical and numerical method in aeroacoustics
title_short Theoretical and numerical method in aeroacoustics
title_sort theoretical and numerical method in aeroacoustics
topic noise
aero-acoustic
discretization
url http://bulletin.incas.ro/files/maria_alexandrescu_v2no2_full.pdf
work_keys_str_mv AT nicusoralexandrescu theoreticalandnumericalmethodinaeroacoustics
AT mariaalexandrescu theoreticalandnumericalmethodinaeroacoustics