Aeroelastic analysis of rotors with trailing edge flaps using comprehensive codes

Journal of the American Helicopter Society

Volumn 46, Issue 3, 2001, Pages 192-199

  Straub, F K ^a   Charles, B D ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; ACTUATORS; FLIGHT DYNAMICS; PIEZOELECTRIC DEVICES; VIBRATION CONTROL;

TRAILING EDGE FLAPS;

ROTORS;

EID: 0035389792     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.46.192     Document Type: Article

References (18)

1. Blade-mounted flap control for BVI noise reduction proof-of-concept test
2. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade
3. Vibration reduction on rotorcraft using active control: A comparison of various approaches
4. Analysis and testing of a machscaled rotor in hover with piezoelectric bender-actuated trailing edge flaps
5. Application of smart materials to control of a helicopter rotor
6. Design of a high efficiency discrete servo-flap actuator for helicopter rotor control
7. Wind tunnel evaluation of a full scale piezoelectric flap control unit
8. Small-scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight
9. Bench-top characterization of an active rotor blade flap system incorporating C-block actuators
10. Aeromechanic considerations in the design of a rotor with smart material actuated trailing edge flaps
11. Application of smart materials to helicopter rotor active control
12. Rotors with trailing edge flaps: Analysis and comparison with experimental data
13. Computation of loads on the McDonnell Douglas advanced bearingless rotor
14. Rotorcraft dynamics models for a comprehensive analysis
15. Higher harmonic actuation of trailing-edge flaps for rotor BVI noise control