A. Gangulee, F.M. D'Heurle
Thin Solid Films
This paper presents a general technique to determine the dynamic response of a plate excited by an orbiting mass. The technique relies on a finite element discretization in which the mesh is consistent with the trajectory of the orbiting mass, combined with a Lagrange multiplier formulation. This allows one to represent the compatibility condition at the mass-plate interface using a set of auxiliary functions. This technique can be applied to plates of any shape, excited by masses describing any type of trajectory. An example is presented to illustrate the method. © 1991.
A. Gangulee, F.M. D'Heurle
Thin Solid Films
S.F. Fan, W.B. Yun, et al.
Proceedings of SPIE 1989
Ellen J. Yoffa, David Adler
Physical Review B
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Journal of Polymer Science Part A: Polymer Chemistry