Investigation in Langley full scale tunnel of stability and control characteristics of convertible type airplane (combination helicopter and airplane) for normal flight attitudes with full power and also for high angles of attack including transition to hovering attitude; comparisons of effects of articulated and rigid propeller operation.


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    Title :

    Static longitudinal stability and control of convertible-type airplane as affected by articulated- and rigid-propeller operation


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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