NASA NTRS · 19890004092
Some nonlinear damping models in flexible structures
Abstract
A class of nonlinear damping models is introduced with application to flexible flight structures characterized by low damping. Approximate solutions of engineering interest are obtained for the model using the classical averaging technique of Krylov and Bogoliubov. The results should be considered preliminary pending further investigation.
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Balakrishnan, A. V.. 1988-10-01. Some nonlinear damping models in flexible structures. https://ntrs.nasa.gov/citations/19890004092
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