Vibration reduction in rotor blades using active composite box beam

AIAA journal

Volumn 38, Issue 7, 2000, Pages 1125-1131

  Chattopadhyay, Aditi ^a   Liu, Qiang ^b   Gu, Haozhong ^c  

^a ARIZONA STATE UNIVERSITY   (United States)

^b Department of Mechanical and Aerospace Engineering ^*

^c Department of Mechanical and Aerospace Engineering

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; CLOSED LOOP CONTROL SYSTEMS; COMPOSITE BEAMS AND GIRDERS; COMPUTER SIMULATION; ELASTICITY; INTELLIGENT MATERIALS; PIEZOELECTRIC DEVICES; SHEAR DEFORMATION; VIBRATION CONTROL;

COMPOSITE BOX BEAM; DYNAMIC DEFORMATION; ROTOR VIBRATORY LOAD ANALYSIS;

HELICOPTER ROTORS;

EID: 0034227472     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1097     Document Type: Article

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