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
1981-10-31
Report
Keine Angabe
Englisch
Autonomous flight control development on the active aeroelastic wing aircraft
Kraftfahrwesen | 2004
|Autonomous Flight Control Development on the Active Aeroelastic Wing Aircraft
SAE Technical Papers | 2004
|