Results of investigation made by Cornell Aeronautical Laboratory are presented; rotor configuration studied utilizes jet-flap for cyclic and collective pitch control as well as for propulsion; effects of blade center-of-gravity position, bending-to-torsional frequency ratio, advance ratio and control-flap characteristics on aeroelastic characteristics of rotor system are reviewed.
Aeroelastic characteristics for jet-flap helicopter rotor in forward flight
SAE -- Paper
SAE Meeting ; 1962
1962
36 pages
Conference paper
English
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THE AEROELASTIC CHARACTERISTICS OF A JET-FLAP HELICOPTER ROTOR IN FORWARD FLIGHT*
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