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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    Titel :

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


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Grunwald, K.J. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    137 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :