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An evaluation of random analysis methods for the determination of panel dampingAn analysis is made of steady-state and non-steady-state methods for the measurement of panel damping. Particular emphasis is placed on the use of random process techniques in conjunction with digital data reduction methods. The steady-state methods considered use the response power spectral density, response autocorrelation, excitation-response crosspower spectral density, or single-sided Fourier transform (SSFT) of the response autocorrelation function. Non-steady-state methods are associated mainly with the use of rapid frequency sweep excitation. Problems associated with the practical application of each method are evaluated with specific reference to the case of a panel exposed to a turbulent airflow, and two methods, the power spectral density and the single-sided Fourier transform methods, are selected as being the most suitable. These two methods are demonstrated experimentally, and it is shown that the power spectral density method is satisfactory under most conditions, provided that appropriate corrections are applied to account for filter bandwidth and background noise errors. Thus, the response power spectral density method is recommended for the measurement of the damping of panels exposed to a moving airflow.
Document ID
19720011259
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bhat, W. V.
(Boeing Co. Seattle, WA, United States)
Wilby, J. F.
(Boeing Co. Seattle, WA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1972
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-114423
Report Number: NASA-CR-114423
Accession Number
72N18909
Funding Number(s)
CONTRACT_GRANT: NAS2-6285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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