Analysis and testing of Mach scaled rotor model with piezoelectric bender actuated trailing-edge flaps for helicopter vibration control

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 1999, Pages 2380-2402

  Koratkar, Nikhil A ^a   Chopra, Inderjit ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT PARTS AND EQUIPMENT; DYNAMIC RESPONSE; EQUIPMENT TESTING; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; VIBRATION CONTROL;

HELICOPTER VIBRATION CONTROL; MACH SCALED ROTOR MODEL; PIEZOELECTRIC BENDER ACTUATED TRAILING EDGE FLAPS;

HELICOPTER ROTORS;

EID: 0032677210     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (24)