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.
Interactive Aircraft Flight Control and Aeroelastic Stabilization
1981
39 pages
Report
No indication
English
Autonomous flight control development on the active aeroelastic wing aircraft
Automotive engineering | 2004
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