This Volume contains plotted trim data obtained from the Boeing Vertol Tandem Rotor Trim and Stability Analysis Program (A-97) for the CH-46E helicopter. Data for the following flight regimes are presented: Level flight; Maximum power climb and autorotation; Constant altitude sideslips; and Sideward flight. For each flight regime considered, the four cockpit control positions, plus helicopter pitch and roll attitudes, are plotted vs. airspeed or sideslip angle.
Helicopter Flying Qualities Characteristics-CH-46E. Volume 2
1983
26 pages
Report
No indication
English
Aeronautics , Aerodynamics , Helicopters , Flight maneuvers , Trim(Aerodynamics) , Experimental data , Flight control systems , Climbing , Autorotation , Sideslip , Airspeed , Pitch(Motion) , Roll , Helicopter rotors , Handling , Quality , Flight envelope , Augmentation , H-46 aircraft , CH-46E aircraft , Flying qualities , Stability augmentation , Tandem flight , Level flight , Sideward flight
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