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Passive control of wing/store flutterResults are presented for a passive flutter suppression approach known as the decoupler pylon. The decoupler pylon dynamically isolates the wing from store pitch inertia effects by means of soft spring/damper elements assisted by a low frequency feedback control system which minimizes static pitch deflections of the store because of maneuvers and changing flight conditions. Wind tunnel tests and analyses show that this relatively simple pylon suspension system provides substantial increases in flutter speed and reduces the sensitivity of flutter to changes in store inertia and center of gravity. Flutter characteristics of F-16 and YF-17 flutter models equipped with decoupler pylon mounted stores are presented and compared with results obtained on the same model configuration with active flutter suppression systems. These studies show both passive and active concepts to be effective in suppressing wing/store flutter. Also presented are data showing the influence of pylon stiffness nonlinearities on wing/store flutter.
Document ID
19810005411
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, W. H., III
(NASA Langley Research Center Hampton, VA, United States)
Cazier, F. W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Foughner, J. T., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
L-14010
NASA-TM-81865
Report Number: L-14010
Report Number: NASA-TM-81865
Meeting Information
Meeting: Joint Tech. Coordinating Group Aircraft Stores Compatibility Symp.,
Location: St. Louis, MO
Country: United States
Start Date: September 9, 1980
End Date: September 11, 1980
Accession Number
81N13922
Funding Number(s)
PROJECT: RTOP 505-33-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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