A reverse #ow theorem for acoustic propagation in compressible potential #ow has been obtained directly from the "eld equations without recourse to energy conservation arguments. A reciprocity theorem for the scattering matrix for the propagation of acoustic modes in a duct with either acoustically
NUMERICAL EXPERIMENTS ON ACOUSTIC RECIPROCITY IN COMPRESSIBLE POTENTIAL FLOWS IN DUCTS
β Scribed by W. EVERSMAN
- Publisher
- Elsevier Science
- Year
- 2001
- Tongue
- English
- Weight
- 340 KB
- Volume
- 246
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
A reciprocity theorem for the scattering matrix for the propagation of acoustic modes in a duct with acoustically hard walls or with acoustically absorbing walls has been given in a companion publication. It was found that for a source at a speci"ed end of the duct, suitably scaled re#ection matrices in direct and reverse #ow have a reciprocal relationship. Scaled transmission matrices obtained for direct #ow and reversed #ow with simultaneous switching of source location from one end to the other also have a reciprocal relationship. A reverse #ow theorem for the equivalent one-dimensional propagation model, which is a good approximation to the three-dimensional model at low frequencies, was also obtained. In this case, using reciprocity and acoustic power conservation arguments it is additionally found that the acoustic power transmission coe$cient is the same for a source at either end of the duct for a given #ow direction. This result leads to an invariance theorem which relates acoustic power propagated due to sources of equal pressure amplitude at the two ends of the duct. A numerical veri"cation of these reciprocal relationships is given here for propagation in axially symmetric (circular and annular) ducts with multi-modal propagation and at low frequencies when a one-dimensional model is appropriate.
π SIMILAR VOLUMES
An experimental and theoretical investigation of the in#uence of a parallel shear #ow on the sound propagation in a circular duct is described. The theoretical model is based on a perturbation expansion at low Mach number of the modal equation for parallel shear #ows (Pridmore-Brown equation). In th
The differential equations governing the transmission of one-dimensional sound waves in a non-uniform duct carrying a subsonic compressible mean flow have been the subject of a recent debate [1,2]. Of the two formulations presented, one is considered to be non-acoustical and the other as neglecting