Paper describes digital program structure input data used, and results produced; complete blade element analyses of main rotor, tail rotor, and propellers are performed throughout maneuver based on instantaneous aerodynamic and dynamic environment; time histories of main rotor blade loads and bending moments are calculated; examples of cases studied, including full autorotative landing, and high-performance deceleration using reversed propeller thrust.
Computer flight testing of rotorcraft
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 10 , n 4
1965
13 pages
Aufsatz (Zeitschrift)
Englisch
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