An aircraft (1) has at least one main wing (2) and at least one boom fuselage (3). The main wing has an aerofoil section having a leading edge (20), a trailing edge (21), a chord length extending between the leading edge and the trailing edge, a centre of lift (Lw), a flexural centre and a centre of mass. The centre of lift, the flexural centre and the centre of mass are located all within a region at most 4% of the chord length.


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    Title :

    Aircraft longitudinal stability



    Publication date :

    2020-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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    ELSON MR ANDREW CHARLES / CAMERON MR DOUGLAS / HORNZEE-JONES MR CHRISTOPHER et al. | European Patent Office | 2018

    Free access

    AIRCRAFT LONGITUDINAL STABILITY

    ELSON ANDREW CHARLES / CAMERON DOUGLAS / HORNZEE-JONES CHRISTOPHER et al. | European Patent Office | 2020

    Free access

    AIRCRAFT LONGITUDINAL STABILITY

    ELSON ANDREW CHARLES / CAMERON DOUGLAS / HORNZEE-JONES CHRISTOPHER et al. | European Patent Office | 2018

    Free access

    AIRCRAFT LONGITUDINAL STABILITY

    ELSON MR ANDREW CHARLES / CAMERON MR DOUGLAS / HORNZEE-JONES MR CHRISTOPHER et al. | European Patent Office | 2020

    Free access

    Aircraft longitudinal stability

    European Patent Office | 2017

    Free access