A wing tip designed for attachment to a winglet of an aircraft, the winglet coupled to a wing of the aircraft and having a leading edge and a trailing edge continuously transitioning from a leading edge and trailing edge of the wing. The wing tip may include a curved leading edge from the winglet leading edge to a leading end point, a curved trailing edge from a winglet trailing edge to a trailing end point, and an end segment connecting the leading end point and the trailing end point. The end segment may be swept back from the trailing end point to the leading end point at an end segment angle.


    Access

    Download


    Export, share and cite



    Title :

    Wing tip with optimum loading


    Contributors:

    Publication date :

    2019-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Wing Tip With Optimum Loading

    GRATZER LOUIS B | European Patent Office | 2019

    Free access

    Wing tip with optimum loading

    GRATZER LOUIS B | European Patent Office | 2016

    Free access

    Wing Tip With Optimum Loading

    GRATZER LOUIS B | European Patent Office | 2017

    Free access

    Optimum Loading of a Wing with a Slit

    Jean-Jacques Chattot | AIAA | 2005


    ENGINEERING NOTES - Optimum Loading of a Wing with a Slit

    Chattot, J.-J. | Online Contents | 2005