Vibration reduction in rotorcraft using the actively controlled trailing edge flap and issues related to practical implementation

Annual Forum Proceedings - American Helicopter Society

Volumn 1, Issue , 1998, Pages 602-619

  Myrtle, Timothy F ^a   Friedmann, Peretz P ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; FAILURE ANALYSIS; FLIGHT DYNAMICS; HELICOPTER ROTORS; MATHEMATICAL MODELS; SYSTEM STABILITY; UNSTEADY FLOW; VIBRATION CONTROL;

ACTIVELY CONTROLLED TRAILING EDGE FLAPS;

HELICOPTERS;

EID: 0031699301     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)