In present paper, Royal Aircraft Establishment test results have been analyzed and are applied to American designs; simpler design criterion, based solely on type and dimensions of tail, has been developed; it is useful in rapid estimation of whether new design is likely to comply with minimum requirements for safety in spinning.


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    Title :

    Approximate spin design criterion for monoplanes


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Seidman, O (author) / Donlan, C.J. (author)


    Publication date :

    1939


    Size :

    7 pages


    Remarks:

    4 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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