Shaoning Yao, Wei-Tsu Tseng, et al.
ADMETA 2011
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.
Shaoning Yao, Wei-Tsu Tseng, et al.
ADMETA 2011
William G. Van der Sluys, Alfred P. Sattelberger, et al.
Polyhedron
Julien Autebert, Aditya Kashyap, et al.
Langmuir
Arvind Kumar, Jeffrey J. Welser, et al.
MRS Spring 2000