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NASA-CR-2682

Fluid mechanical model of the acoustic impedance of small orifices

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1975

Abstract: A fluid mechanical model of the acoustic behavior of small orifices is presented which predicts orifice resistance and reactance as a function of incident sound pressure level, frequency, and orifice geometry. Agreement between predicted and measured values is excellent. The model shows the following: (1) The acoustic flow in immediate neighborhood of the orifice can be modeled as a locally spherical flow. Within this near field, the flow is, to a first approximation, unsteady and incompressible. (2) At very low sound pressure levels, the orifice viscous resistance is directly related to the effect of boundary-layer displacement along the walls containing the orifice, and the orifice reactance is directly related to the inertia of the oscillating flow in the neighborhood of the orifice. (3) For large values of the incident acoustic pressure, the impedance is dominated by nonlinear jet-like effects. (4) For low values of the pressure, the resistance and reactance are roughly equal.
URI: https://yse.yabesh.ir/std/handle/yse/107177
Subject: ACOUSTIC
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-CR-2682

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:43:50Z
date available2017-09-04T16:43:50Z
date copyright01/01/1975
date issued1975
identifier otherVVMKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/107177
description abstractA fluid mechanical model of the acoustic behavior of small orifices is presented which predicts orifice resistance and reactance as a function of incident sound pressure level, frequency, and orifice geometry. Agreement between predicted and measured values is excellent. The model shows the following: (1) The acoustic flow in immediate neighborhood of the orifice can be modeled as a locally spherical flow. Within this near field, the flow is, to a first approximation, unsteady and incompressible. (2) At very low sound pressure levels, the orifice viscous resistance is directly related to the effect of boundary-layer displacement along the walls containing the orifice, and the orifice reactance is directly related to the inertia of the oscillating flow in the neighborhood of the orifice. (3) For large values of the incident acoustic pressure, the impedance is dominated by nonlinear jet-like effects. (4) For low values of the pressure, the resistance and reactance are roughly equal.
languageEnglish
titleNASA-CR-2682num
titleFluid mechanical model of the acoustic impedance of small orificesen
typestandard
page58
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsACOUSTIC
subject keywordsFLOW
subject keywordsFLUID
subject keywordsIMPEDANCE
subject keywordsMATHEMATICAL
subject keywordsMECHANICS
subject keywordsMODELS
subject keywordsNONLINEAR
subject keywordsORIFICE
subject keywordsORIFICES
subject keywordsPRESSURE
subject keywordsREACTANCE
subject keywordsRESISTANCE
subject keywordsSOUND
subject keywordsSYSTEMS
subject keywordsTRANSMISSION
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