NASA NTRS · 19820005277
Interactive aircraft flight control and aeroelastic stabilization
Abstract
Several 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.
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Weisshaar, T. A., Schmidt, D. K.. 1981-10-31. Interactive aircraft flight control and aeroelastic stabilization. https://ntrs.nasa.gov/citations/19820005277
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