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YF-16 flight flutter test proceduresThe Random Decrement technique (Randomdec) was incorporated in procedures for flight testing of the YF-16 lightweight fighter prototype. Damping values obtained substantiate the adequacy of the flutter margin of safety. To confirm the structural modes which were being excited, a spectral analysis of each channel was performed using the AFFTC time/data 1923/50 time series analyzer. Inflight test procedure included the careful monitoring of strip charts, three axis pulses, rolls, and pullups.
Document ID
19770014094
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brignac, W. J.
(General Dynamics/Fort Worth TX, United States)
Ness, H. B.
(General Dynamics/Fort Worth TX, United States)
Johnson, M. K.
(General Dynamics/Fort Worth TX, United States)
Smith, L. M.
(General Dynamics/Fort Worth TX, 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
77N21038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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