Thomas H. Baum, Carl E. Larson, et al.
Journal of Organometallic Chemistry
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 H. Baum, Carl E. Larson, et al.
Journal of Organometallic Chemistry
Sang-Min Park, Mark P. Stoykovich, et al.
Advanced Materials
William Hinsberg, Joy Cheng, et al.
SPIE Advanced Lithography 2010
M.A. Lutz, R.M. Feenstra, et al.
Surface Science