Vibration reduction in hingeless rotors using an actively controlled trailing edge flap: implementation and time domain simulation

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

Volumn 1, Issue , 1994, Pages 8-22

  Millott, Thomas A ^a   Friedmann, Peretz P ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CONTROL SYSTEMS; DRAG; DYNAMIC RESPONSE; FEEDBACK CONTROL; FREQUENCY DOMAIN ANALYSIS; LOADS (FORCES); MATRIX ALGEBRA; TIME DOMAIN ANALYSIS; TRANSFER FUNCTIONS; VECTORS; VIBRATION CONTROL;

BLADE MODEL; HINGELESS ROTORS; POWER EFFICIENCY; SPANWISE LOCATION; TORSIONAL STIFFNESS; TRAILING EDGE FLAP; VIBRATION REDUCTION;

HELICOPTER ROTORS;

EID: 0028695920     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (37)