Helicopter horizontal tail incidence control to reduce rotor cyclic pitch and blade flapping

Annual Forum Proceedings - American Helicopter Society

Volumn 1, Issue , 2004, Pages 1098-1119

  Gandhi, Farhan ^a,c   Sekula, Martin K ^b  

^a The Pennsylvania State University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Penn Stt Rotorcraft Ctr Excellence   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLADE FLAPPING; CYCLIC PITCH; DYNAMIC STRESSES;

COMPUTER SIMULATION; DEFLECTION (STRUCTURES); DRAG; GRAVITATION; PIEZOELECTRICITY; SHAFTS (MACHINE COMPONENTS); STRESSES;

HELICOPTER ROTORS;

EID: 4143083696     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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