The attenuation of a plane acoustic wave incident on a flat impedance surface in a sheared and viscous fluid is investigated numerically and asymptotically. Predictions of various boundary models of impedance surfaces in shear flow are tested by comparing their predicted reflection coefficient. It is found that viscosity has a significant effect, reducing the reflection of upstream propagating sound while increasing the reflection of cross-stream propagating sound. The classical Ingard-Myers boundary condition is shown to incorrectly predict the damping rate of sound in many cases, and in some cases viscous effects are shown to be comparable to shear effects
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
International audienceA theoretical description of ideal and viscous fluid media is proposed to addr...
The effect of viscosity and thermal conduction on the acoustics in a shear layer above an impedance ...
The acoustics of a mean flow boundary layer over an impedance surface or acoustic lining is consider...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
Although the acoustic analogy developed by Lighthill, Curle, and Ffowcs Williams and Hawkings for so...
In principle, the impedance of a locally reacting acoustic liner should be independent of the struct...
Impedance eduction experiments on acoustic liners with flow have systematically shown the educed imp...
This paper considers the effects of a thin laminar compressible viscous boundary layer over acoustic...
AbstractThe viscosity of the medium plays an important role in defining the characteristics of sound...
Acoustic liners remain a key technology for reducing community noise from aircraft engines. The choi...
The interpretation of unsteady surface shear stresses as dipole sound sources is discussed. Provided...
The unsteady axisymmetric flow through a circular aperture in a thin plate subjected to harmonic for...
This paper presents results of an investigation of the effects of shear flow profile on impedance ed...
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
International audienceA theoretical description of ideal and viscous fluid media is proposed to addr...
The effect of viscosity and thermal conduction on the acoustics in a shear layer above an impedance ...
The acoustics of a mean flow boundary layer over an impedance surface or acoustic lining is consider...
New noise regulations for civil aviation restrict the sound level that engines can emit to a great e...
Although the acoustic analogy developed by Lighthill, Curle, and Ffowcs Williams and Hawkings for so...
In principle, the impedance of a locally reacting acoustic liner should be independent of the struct...
Impedance eduction experiments on acoustic liners with flow have systematically shown the educed imp...
This paper considers the effects of a thin laminar compressible viscous boundary layer over acoustic...
AbstractThe viscosity of the medium plays an important role in defining the characteristics of sound...
Acoustic liners remain a key technology for reducing community noise from aircraft engines. The choi...
The interpretation of unsteady surface shear stresses as dipole sound sources is discussed. Provided...
The unsteady axisymmetric flow through a circular aperture in a thin plate subjected to harmonic for...
This paper presents results of an investigation of the effects of shear flow profile on impedance ed...
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
La première partie concerne les interactions acoustique-vorticité dans les écoulements cisaillés lin...
International audienceA theoretical description of ideal and viscous fluid media is proposed to addr...