A 6 ร 6 transfer matrix is presented to evaluate the response of a multi-layered infinitely long elastic cylinder, imbedded in a fluid and enclosing another fluid, to a given two-dimensional pressure excitation on the outside or inside, or alternatively to evaluate the acoustic pressure distribution
RESPONSE OF A MULTI-LAYERED INFINITE CYLINDER TO A PLANE WAVE EXCITATION BY MEANS OF TRANSFER MATRICES
โ Scribed by J.S. Sastry; M.L. Munjal
- Publisher
- Elsevier Science
- Year
- 1998
- Tongue
- English
- Weight
- 309 KB
- Volume
- 209
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
A 4 ร 4 transfer matrix is derived to evaluate the response of a multi-layered infinitely long elastic cylinder imbedded in a fluid and enclosing another fluid, to a given one-dimensional pressure excitation, or alternatively to evaluate the acoustic pressure distribution excited by the radial velocity component of the radiating surface. It is shown that the transfer matrix can be effectively used to obtain the scattering coefficient and noise reductiion of a multi-layered cylinder for the case of normal incidence of a plane wave. Expressions for several particular cases, such as monostatic back scattering, scattering from a rigid cylinder and a soft cylinder, a solid and a fluid cylinder, are presented. It is shown analytically that the expressions for scattering coefficient for the general case of a hollow cylinder and the particular cases of a fluid cylinder and a solid cylinder lead to the same expressions obtained by using a normal mode solution. Numerical results for the scattering form function and noise reduction of a two-layer infinite cylinder are given to illustrate the effect of layer material characteristics, variation of thickness of either of the constituent layers, cylinder dimensions, and ambient media. Finally, a four-layer hose has been analyzed in order to demonstrate the computational advantage of the transfer matrix method.
๐ SIMILAR VOLUMES
Starting with the basic equations connecting the state variables of normal stress, shear stress, tangential velocity and normal velocity, a transfer matrix for a solid plate has been derived. It has been shown that for the limiting case of normal excitation (tangential wave number equalling zero), t
A 6 ร 6 transfer matrix is presented to evaluate the response of a multi-layer infinite plate to a given two-dimensional pressure excitation on one of its faces or, alternatively, to evaluate the acoustic pressure distribution excited by the normal velocity components of the radiating surfaces. It i