Helicopter Vibration and Rotor Power Reduction through Horizontal Tail Incidence Angle Control
Annual forum; 60th, American Helicopter Society; 60th annual forum proceedings ; 2004 ; Baltimore, MD
2004-01-01
15 pages
Part 2 of 2
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade Flapping
British Library Conference Proceedings | 2004
|Vibration reduction sand box structure of horizontal tail of helicopter and helicopter
European Patent Office | 2024
|INTERMESHING DUAL-ROTOR HELICOPTER AND HORIZONTAL TAIL CONTROL SYSTEM
European Patent Office | 2023
|Helicopter horizontal tail stepless angle adjusting tilting mechanism
European Patent Office | 2023
|