Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade Flapping
Annual forum; 60th, American Helicopter Society; 60th annual forum proceedings ; 2004 ; Baltimore, MD
01.01.2004
22 pages
Part 1 of 2
Aufsatz (Konferenz)
Englisch
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Helicopter Rotor Blade Flapping and Bending
Emerald Group Publishing | 1957
|Helicopter Rotor Blade Flapping and Bending
Emerald Group Publishing | 1957
|Helicopter Vibration and Rotor Power Reduction through Horizontal Tail Incidence Angle Control
British Library Conference Proceedings | 2004
|