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Turbulence excited frequency domain damping measurement and truncation effectsExisting frequency domain modal frequency and damping analysis methods are discussed. The effects of truncation in the Laplace and Fourier transform data analysis methods are described. Methods for eliminating truncation errors from measured damping are presented. Implications of truncation effects in fast Fourier transform analysis are discussed. Limited comparison with test data is presented.
Document ID
19770014083
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soovere, J.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Flutter Testing Tech.,
Subject Category
Aircraft Design, Testing And Performance
Accession Number
77N21027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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