Method of determining approximately conditions in which it is necessary to automatically balance moment of propeller thrust by supplementary moment of empennage; determining rapidly best possible position of center of gravity to give sufficient stability without placing exaggerated stress on stabilizer and elevators; effect of slipstream of wing and propeller on fuselage.


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    Title :

    Method of calculating the horizontal tail surfaces of an airplane


    Additional title:

    Abaque pour le calcul de l'empennage horizontal d'un avion


    Contributors:
    Lepe&grave (author) / re, G. (author)

    Published in:

    Aeronautique ; 11 , n 116 ; p 11-18


    Publication date :

    1929


    Size :

    8 pages


    Remarks:

    6 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    French


    Keywords :



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