Requirements for tail surfaces that would provide effective control for satisfactory recovery from fully developed spins have been determined from analysis of characteristics of approximately 60 models previously tested in Langley spin tunnels. See also Engineering Index 1946 p 24.


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    Title :

    Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    8 pages


    Remarks:

    3 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English