Add to ORKGFlight test with large helicopter showing trends of lateral and longitudinal control response with siz
Helicopter flight investigation of effects of gross changes in static directional stability on v/sto...
A study of helicopter roll control effectiveness based on closed-loop task performance measurement a...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
Optimum values of pitch rate damping, longitudinal control and speed stability for vertical takeoff ...
Measured and predicted dynamic response characteristics of a large flexible swept-wing airplane to c...
A piloted simulation experiment conducted on the NASA-Ames Vertical Motion Simulator evaluated the h...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
A helicopter in-flight simulation was conducted to determine the effects of variations in roll dampi...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
A joint U.S. Army/NASA flight investigation was conducted utilizing a single-rotor helicopter to det...
A current preoccupation of the designers of fixed-wing aircraft is the extent to which ACT might all...
Flight tests on hingeless rotor compound helicopter to determine level flight and maneuvering charac...
Wind tunnel investigation of helicopter directional control in rearward flight in ground effec
In recent years, NASA has invested in key activities in the areas of flight controls, handling quali...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
Helicopter flight investigation of effects of gross changes in static directional stability on v/sto...
A study of helicopter roll control effectiveness based on closed-loop task performance measurement a...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
Optimum values of pitch rate damping, longitudinal control and speed stability for vertical takeoff ...
Measured and predicted dynamic response characteristics of a large flexible swept-wing airplane to c...
A piloted simulation experiment conducted on the NASA-Ames Vertical Motion Simulator evaluated the h...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
A helicopter in-flight simulation was conducted to determine the effects of variations in roll dampi...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
A joint U.S. Army/NASA flight investigation was conducted utilizing a single-rotor helicopter to det...
A current preoccupation of the designers of fixed-wing aircraft is the extent to which ACT might all...
Flight tests on hingeless rotor compound helicopter to determine level flight and maneuvering charac...
Wind tunnel investigation of helicopter directional control in rearward flight in ground effec
In recent years, NASA has invested in key activities in the areas of flight controls, handling quali...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
Helicopter flight investigation of effects of gross changes in static directional stability on v/sto...
A study of helicopter roll control effectiveness based on closed-loop task performance measurement a...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...