In most turbofan engine intakes, the acoustically lined region consists of several liner segments which are separated by longitudinal hard-walled intercostal strips or splices. Measurements indicate that the duct modal spectrum can be considerably altered by such circumferential variations in acoust
Influence of liner thickness on wave propagation in ducts
โ Scribed by J.E. Kaiser; B.S. Shaker; A.H. Nayfeh
- Publisher
- Elsevier Science
- Year
- 1974
- Tongue
- English
- Weight
- 706 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
The acoustic characteristics of a point-reacting duct liner that consists of a porous facing sheet backed by cellular cavities are derived by examining the wave propagation within the liner. The relation between the derived expression for the liner acoustic admittance and a semi-empirical formula that is widely used in the literature is discussed. The influence of the liner on acoustic propagation in a duct is examined for the case of a plane duct that carries a uniform mean flow. Numerical results for the attenuation rates vs. frequency are presented. These results are of three types: (a) comparisons with previously published results for no backing cavity and no mean flow are made, and these results are extended to include the effects of the mean flow; (b) results of parametric variations of the liner dimensions are presented to assess the relative influences of the facing-sheet thickness and the cavity depth; (c) results from the derived expression for liner specific admittance and from the semi-empirical formula are compared in order to determine the significance of the wave propagation within the porous material and to determine the range of validity of the semi-empirical formula.
๐ 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