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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Neihouse, A.I. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    8 pages


    Anmerkungen:

    3 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch