Characteristics of aircraft during transition from hovering to normal flight are studied measuring longitudinal, lateral, and directional stability and control characteristics; data are used for simulation to document handling qualities of vehicle; it is concluded that aircraft could perform transition within certain boundaries.


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    Titel :

    Wind-tunnel and piloted flight simulator investigation of deflected-slipstream VTOL airplane, ryan VZ-3ry


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    James, H.A. (Autor:in) / Wingrove, R.C. (Autor:in) / Holzhauser, C.A. (Autor:in) / Drinkwater III, F.J. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    88 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :