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TECHNICAL PAPERS

Identification of Multi-Degree of Freedom Systems With Nonproportional Damping Using the Resonant Decay Method

[+] Author and Article Information
Steven Naylor

ArvinMeritor Inc., Warton Technical Center, Hillock Lane, Warton, Preston, Lancashire, PR4 1TP UKe-mail: steven.naylor@arvinmeritor.com

Michael F. Platten, Jan R. Wright, Jonathan E. Cooper

School of Engineering, University of Manchester, Oxford Road, Manchester, M13 9PL, UK

J. Vib. Acoust 126(2), 298-306 (May 04, 2004) (9 pages) doi:10.1115/1.1687395 History: Received April 01, 2002; Revised August 01, 2003; Online May 04, 2004
Copyright © 2004 by ASME
Topics: Force , Damping , Stiffness , Errors , Shapes
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References

Figures

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Plate model dimensions and measurement positions
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Modified MMIF eigenvalues for two exciters and non-proportional damping (Case A)
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Modal forces and responses for the burst appropriation of mode 2 (Case A—no error)
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Modal forces and responses for the burst appropriation of mode 3 (Case A—no error)
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Modal forces and responses for the burst appropriation of mode 5 (Case A—no error)
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Modal forces and responses for the burst appropriation of mode 1 (Case D—appropriation error)
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Modal forces and responses for the burst appropriation of mode 2 (Case F—mode shape error)

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