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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    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    88 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :