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Decoupler pylon - A simple, effective wing/store flutter suppressorAs an alternative to alleviating wing/store flutter by conventional passive methods or by more advanced active control methods, a quasi-passive concept, referred to as the decoupler pylon, is investigated which combines desirable features of both methods. Passive soft-spring/damper elements are used to decouple wing modes from store pitch modes, and a low-power control system maintains store alignment under changing mean loads. It is shown by analysis and wind tunnel tests that the decoupler pylon provides substantial increase in flutter speed and makes flutter virtually insensitive to inertia and center-of-gravity location of the store.
Document ID
19790045022
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Reed, W. H.
(NASA Langley Research Center Hampton, VA, United States)
Foughner, J. T., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Runyan, H. L., Jr.
(George Washington University Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 79-0791
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials Conference
Location: St. Louis, MO
Start Date: April 4, 1979
End Date: April 6, 1979
Accession Number
79A29035
Distribution Limits
Public
Copyright
Other

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