𝔖 Bobbio Scriptorium
✦   LIBER   ✦

TRANSIENT ACOUSTIC DIFFRACTION AND RADIATION BY AN AXISYMMETRICAL ELASTIC SHELL: A NEW STATEMENT OF THE BASIC EQUATIONS AND A NUMERICAL METHOD BASED ON POLYNOMIAL APPROXIMATIONS

✍ Scribed by C. MAURY; P.J.T. FILIPPI


Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
408 KB
Volume
241
Category
Article
ISSN
0022-460X

No coin nor oath required. For personal study only.

✦ Synopsis


This work deals with an axisymmetrical shell composed of a cylindrical shell closed by two hemispherical shells made of the same material and with the same thickness. The shell is immersed into a homogeneous perfect #uid extending to in"nity. The "rst part is devoted to the establishment of the equations governing the shell vibrations. The method used, which, in the authors' opinion, is not quite new, is based on the expansion of the elasticity equations into a Taylor series of the transverse variable: by using the same degree of expansion, the equations obtained for the cylindrical part and for the spherical parts are consistent (they correspond to the Donnell and Mushtari approximation). The "rst interest of this analysis is that the continuity conditions along the junction lines between the cylindrical and the spherical parts are immediately obtained. The main problem is to obtain the boundary conditions satis"ed by the hemispherical shells displacement at the apexes. Indeed, due to the use of spherical co-ordinates*which is a quite natural choice*the coe$cients of the equations become singular at the apexes and boundary conditions are required to express that an apex is a mechanically regular point. The method that is used here enables one to obtain such a result which, to the authors' knowledge, is new. The transient response of the system shell/external #uid is sought as a series of its resonance modes, that is its free oscillations. The main di$culty is to obtain a numerical approximation of the resonance modes: their calculation leads to solving the Fourier transform of the system of homogeneous equations. The numerical method for solving the problem is the following. The acoustic pressure is described by a hybrid layer potential, the density of which is approximated by a linear combination of orthogonal polynomials. Each component of the shell displacement is approximated by a linear combination of polynomial functions: these functions are chosen as linear combinations of orthogonal polynomials which satisfy the same continuity and boundary conditions as the shell displacement components. In the "rst step, the resonance frequencies are calculated. Then the coe$cients of the corresponding resonance mode expansion are deduced. The validity and the e$ciency of this approach will be shown in a second article through comparisons between numerical predictions and experimental results.