NASA NTRS · 19870028657
A procedure for calculating the damping in multi-element space structures
Abstract
A procedure for analyzing the damping in a multielement space structure connected by joints is described, in which distributed material damping and discrete nonlinear joint properties are incorporated into a linear analysis. The procedure involves four steps: (1) creation of a linear undamped finite element model; (2) experimental measurements of the transient response of a truss member in free fall tests to obtain material damping properties; with these properties incorporated into a linear damped finite element model of the structure; (3) the identification of the nonlinear joint properties using the force-state mapping technique; and (4) linearization of the identified nonlinear components, which are then incorporated into the linear damped model to create the linearized damped finite element model.
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Crawley, E. F., Odonnell, K. J.. 1986-10-01. A procedure for calculating the damping in multi-element space structures. https://ntrs.nasa.gov/citations/19870028657
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