Airplane tail surface design that would make recoveries from spins satisfactory was investigated in analysis of characteristics of models of approximately 100 military airplanes; relative distribution of mass along wings and fuselage, relative density of airplane, and design of vertical surfaces, considered.


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    Titel :

    Tail-design requirements for satisfactory spin recovery


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Neihouse, A.I. (Autor:in) / Lichtenstein, J.H. (Autor:in) / Pepoon, P.W. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    8 pages


    Anmerkungen:

    Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Tail-design requirements for satisfactory spin recovery

    Neihouse, Jacob H / Lichtenstein, Jacob H / Pepoon, Philip W | NTRS | 1946



    Requirements for satisfactory flying qualities

    Blom, J.H.D. | Engineering Index Backfile | 1949