Small-scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight

Annual Forum Proceedings - American Helicopter Society

Volumn 1, Issue , 1998, Pages 433-451

  Fulton, Mark V ^a   Ormiston, Robert A ^a  

^a US Army Aviation RD&E Cent   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AERODYNAMICS; BENDING (DEFORMATION); DYNAMIC RESPONSE; FLIGHT DYNAMICS; FREQUENCY RESPONSE; STRUCTURAL ANALYSIS; TORSIONAL STRESS; VIBRATION CONTROL; WIND TUNNELS;

BLADE VIBRATORY LOADS; HARMONIC BLADE VIBRATORY FLAP BENDING MOMENTS; ON BLADE ELEVONS;

HELICOPTER ROTORS;

EID: 0031651091     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)