Flight and wind tunnel tests were conducted and multidiscipline computer programs were developed as part of investigations of active control technology conducted at the NASA Langley Research Center. Unsteady aerodynamics approximation, optimal control theory, optimal controller design, and the Delta wing and DC-10 models are described. The drones for aerodynamics and structural testing (DAST program) for evaluating procedures for aerodynamic loads prediction and the design of active control systems on wings with significant aeroelastic effects is described as well as the DAST model used in the wind tunnel tests.
Some experiences with active control of aeroelastic response
1981-07-01
Report
No indication
English
Active control of aeroelastic response
NTRS | 1972
|CFD-based aeroelastic response of an active aeroelastic wing
Tema Archive | 2004
|