Helicopter performance and vibration enhancement by twist-actuated blades

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

Volumn 5, Issue , 2003, Pages 3891-3901

  Shin, SangJoon ^a   Cesnik, Carlos E S ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ALGORITHMS; CLOSED LOOP CONTROL SYSTEMS; COMPOSITE STRUCTURES; CONTROL SYSTEM ANALYSIS; PERFORMANCE; PIEZOELECTRIC MATERIALS; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL); WIND TUNNELS;

LANGLEY TRANSONIC DYNAMIC TUNNELS; PAYLOAD; TWIST ACTUATED BLADES; VIBRATION ENHANCEMENT; VIBRATORY LOADS;

HELICOPTERS;

EID: 0042009869     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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