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    Thrust augmented spin recovery device (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Format: application/pdf
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