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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    Titel :

    Approximate spin design criterion for monoplanes


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Seidman, O (Autor:in) / Donlan, C.J. (Autor:in)


    Erscheinungsdatum :

    1939


    Format / Umfang :

    7 pages


    Anmerkungen:

    4 Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    An approximate spin design criterion for monoplanes

    Seidman, Oscar / Donlan, Charles J. | TIBKAT | 1940


    An approximate spin design criterion for monoplanes

    Seidman, Oscar ;Donlan, Charles J. | SLUB | 1939


    The Ryan Monoplanes

    Emerald Group Publishing | 1941


    Ryan monoplanes

    Engineering Index Backfile | 1941


    Sablatnig monoplanes

    Langsdorff, Werner v. | Engineering Index Backfile | 1920