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Interactive aircraft flight control and aeroelastic stabilizationSeveral examples are presented in which flutter involving interaction between flight mechanics modes and elastic wind bending occurs for a forward swept wing flight vehicle. These results show the basic mechanism by which the instability occurs and form the basis for attempts to actively control such a vehicle.
Document ID
19820005277
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weisshaar, T. A. (Purdue Univ. West Lafayette, IN, United States)
Schmidt, D. K. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 4, 2013
Publication Date
October 31, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-165036
Report Number: NASA-CR-165036
Accession Number
82N13150
Funding Number(s)
CONTRACT_GRANT: NAG1-157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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