Longitudinal and lateral stability and control characteristics were investigated from hovering to forward flight; tests covered pure tilt wing, tilt wing with flap, slats, wing span extension, and tilt wing with speed brakes and slats; tests were conducted in and out of ground effect and included investigation of stabilizer and tail fan effectiveness.


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    Title :

    Aerodynamic characteristics of four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    137 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :