Yaw control surfaces were developed for a jet propelled aircraft. A thrust augmented rudder is disposed above the jet exhaust stream and a thrust rudder tab extends downward into the jet exhaust stream. These components are cooperatively deflected to generate yawing moments for directional control of the aircraft.
Thrust augmented spin recovery device
1980-12-02
Sonstige
Keine Angabe
Englisch
Thrust Augmented Spin Recovery Device
NTIS | 1979
|Thrust Augmented Spin Recovery Device
NTIS | 1976
|Thrust Augmented Spin Recovery Device
NTIS | 1979
|Thrust-augmented vortex attenuation
NTRS | 1977
|Wingtip Vortex-Augmented Turbopusher Propeller Thrust
NTRS | 1985
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