Open-loop hover testing of a smart rotor model

AIAA Journal

Volumn 40, Issue 8, 2002, Pages 1495-1502

  Koratkar, Nikhil A ^a   Chopra, Inderjit ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AMPLIFICATION; ELECTRIC POTENTIAL; NATURAL FREQUENCIES; OPTIMIZATION; OSCILLATORS (MECHANICAL); PIEZOELECTRIC DEVICES; RESONANCE; STRESSES; TORSIONAL STRESS; VIBRATION CONTROL;

ACTUATOR RESONANT AMPLIFICATION; ACTUATOR-FLAP SYSTEMS;

HELICOPTER ROTORS;

EID: 0036684208     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1834     Document Type: Article

References (21)

1. Full-scale wind tunnel test of a helicopter individual blade control system
2. Design and first flight tests of individual blade control actuators
3. Design of a servo-flap rotor for reduced control loads
4. Analysis and testing of a Froude-scaled rotor with piezolectric bender actuated trailing-edge flaps
5. Hover testing of a small-scale rotor with on-blade elevons
6. Design and spin testing of an active trailing-edge flap actuated with Piezo-stacks
7. Design and experimental testing of an induced-shear piezoelectric actuator for rotor blade trailing-edge flaps
8. Hover testing of an active rotor blade tip
9. Development of a smart rotor blade with induced strain actuation of blade twist
10. Design and manufacture of an integral-twist actuated rotor blade
11. Hover testing of the NASA/ARL/MIT active twist rotor
12. Wind tunnel testing of a mach-scaled rotor model with trailing-edge flaps
13. Analysis and testing of mach-scaled rotor with trailing-edge flaps