Stability and control characteristics of a four propeller tilt wing vtol model with programmed flap


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    Title :

    FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMED FLAP


    Contributors:

    Publication date :

    1962-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English