Active vibration suppression systems applied to twin tail buffeting

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 3326, Issue , 1998, Pages 27-33

  Hopkins, Mark ^a   Henderson, Doug ^a   Moses, Robert ^a   Ryall, Tom ^a   Zimcik, David ^a   Spangler, Ron ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Active control; Aircraft; Buffet; Piezoelectric; Vibration

Indexed keywords

AERODYNAMICS; DRAG; LIFT; PIEZOELECTRICITY; VIBRATION CONTROL;

VIBRATION SUPPRESSION SYSTEMS;

BUFFETING;

EID: 0032401298     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.310663     Document Type: Conference Paper

References (20)

1. Wind tunnel investigation and flight tests of tail buffet on the CF-18 aircraft
2. Full-scale wind-tunnel pressure measurements on an F/A-18 tail during buffet
3. Full-scale wind-tunnel studies of F/A-18 tail buffet
4. The application of dynamic loads to a full scale F/A-18 fatigue test article
5. Progress and new techniques in buffet alleviation
6. Vortex control technique for the attenuation of fin buffet
7. Tangential leading-edge blowing on a combat aircraft configuration
8. Investigation of buffet load alleviation on a scaled F-15 twin tail model
9. Conceptual design of damping treatments for the F/A-18 vertical tail
10. Integral damping treatment for primary aircraft structures
11. Composite 'Exoskin' doubler extends F-15 vertical tail fatigue life
12. Active control for fin buffet alleviation
13. An active smart material system for buffet load alleviation
14. Vertical tail buffeting alleviation using piezoelectric actuators - Some results of the actively controlled response of buffet-affected tails (ACROBAT) program
15. Active vertical tail buffeting alleviation on a twin-tail fighter configuration in a wind tunnel
16. Reduction of vertical tail buffet response using active control
17. Single actuator and multi-mode acceleration feedback control
18. Active load alleviation technology
19. Buffet load alleviation using distributed piezoelectric actuators