The stability conditions of Ente (duck) airplanes are investigated in this report. In developing the formulas, which afford an approximate solution, the unimportant effect of the height of the C.G. and the moment of the residual resistance are neglected. The effect of downwash from the forward horizontal empennage on the wing are also disregarded.


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    Title :

    Static longitudinal stability of "Ente" airplanes


    Contributors:

    Publication date :

    1931-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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