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Some experience using subcritical response methods in wind-tunnel flutter model studiesExperiences obtained with four methods of predicting flutter of wind-tunnel models from subcritical response data are described. The four methods are: co/quad, randomdec, power spectra density, and the peak-hold spectrum. Model excitation techniques included both forced (sinusoidal sweep) and random (tunnel turbulence). These methods were successfully used to measure the frequency and damping (or an inverse response amplitude proportional to the damping) in the predominant flutter modes. Implementation and application of each method are discussed. Some results and comparisons between methods are presented.
Document ID
19770014085
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Foughner, J. T., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Flutter Testing Tech.,
Subject Category
Aircraft Design, Testing And Performance
Accession Number
77N21029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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