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Vector plotting as an indication of the approach to flutterA binary flexure-torsion analysis was made to check theoretically a method for predicting flutter which depends on plotting vectorially the amplitudes of response relative to the exciting force and extracting the relevant damping rate. The results of this calculation are given in graphs both of the vector plots themselves and of the estimated damping rate against forward speed. The estimated damping rates are compared with calculated values. The method has the advantage that in a flight flutter test damping can be estimated from continuous excitation records: the method is an extension of the Kennedy and Pancu technique used in ground resonance testing.
Document ID
19760003012
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Broadbent, E. G.
(Royal Aircraft Establishment Farnborough, United Kingdom)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA, Washington Flight Flutter Testing Symp.
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N10100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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