Thomas E. Karis, C. Mark Seymour, et al.
Rheologica Acta
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.
Thomas E. Karis, C. Mark Seymour, et al.
Rheologica Acta
J.R. Thompson, Yang Ren Sun, et al.
Physica A: Statistical Mechanics and its Applications
S. Cohen, T.O. Sedgwick, et al.
MRS Proceedings 1983
O.F. Schirmer, K.W. Blazey, et al.
Physical Review B