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Some nonlinear damping models in flexible structuresA 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.
Document ID
19890004092
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Balakrishnan, A. V. (California Univ. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Publication Information
Publication: NASA, Langley Research Center, Proceedings of the 4th Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89N13463
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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