| contributor author | W. Gafsi | |
| contributor author | S. Choura | |
| contributor author | A. Nayfeh | |
| date accessioned | 2017-05-08T21:16:30Z | |
| date available | 2017-05-08T21:16:30Z | |
| date copyright | October 2009 | |
| date issued | 2009 | |
| identifier other | %28asce%290893-1321%282009%2922%3A4%28403%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45185 | |
| description abstract | A strategy for confinement of flexural vibrations in flexible structures by proper selection of their geometrical and physical parameters is proposed. We first show that the problem of vibration confinement can be formulated as an inverse eigenvalue problem (IEP) where the mode shapes and/or natural frequencies are assumed and the geometrical and physical properties are unknown functions of the space variables. It is required that the assumed modes form a complete and independent set of spatial functions that satisfy the boundary conditions and guarantee confinement within the desired spatial subdomain(s) of the structure. Using simple spatial functions, such as polynomials and exponentials, we determined approximate solutions of the geometrical and physical parameters by applying the orthogonality of the mode shapes with respect to the stiffness and mass density. The order of the selected polynomials or exponentials depends on the number of modes retained in the discretized model. Numerical simulations are presented on a beam and then on a plate to examine convergence of the solution to the IEP. We show that convergence is attained with few assumed mode shapes. The approximated parameters are finally substituted into the forward eigenvalue problem to confirm confinement at the desired locations. | |
| publisher | American Society of Civil Engineers | |
| title | Assignment of Geometrical and Physical Parameters for the Confinement of Vibrations in Flexible Structures | |
| type | Journal Paper | |
| journal volume | 22 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2009)22:4(403) | |
| tree | Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 004 | |
| contenttype | Fulltext | |