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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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


    Publication date :

    1929


    Size :

    8 pages


    Remarks:

    6 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    French


    Keywords :



    Airplane horizontal tail connecting mechanism bush installation method

    SUN FEI / WANG YINGHOU / LI SEN et al. | European Patent Office | 2022

    Free access



    Airplane horizontal tail elevator maneuverability test device and method thereof

    ZANG WEIFENG / CHENG HUA / CHEN AN et al. | European Patent Office | 2023

    Free access