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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    Title :

    Tail-design requirements for satisfactory spin recovery


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1946


    Size :

    8 pages


    Remarks:

    Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Tail-design requirements for satisfactory spin recovery

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



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



    Requirements for satisfactory flying qualities of airplanes

    Gilruth, R.R. | Engineering Index Backfile | 1947