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
1979
6 pages
Report
No indication
English
Aerodynamics , Aircraft , Government Inventions for Licensing , Patents , Aerial rudders , Attitude control , Spin stabilization , Thrust augmentation , Yaw , Aerodynamic stability , Aircraft structures , Flight control , Secondary injection , Turning flight , Yawing moments , PAT-CL-244-52 , PAT-CL-244-87 , PAT-CL-244-12.5
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