An airfoil for an aircraft having an airfoil geometry. The airfoil geometry includes an upper surface and a lower surface, the upper and lower surfaces are in accordance with Cartesian coordinate values of X and Y. The Cartesian coordinate values of X and Y are non-dimensional values from 0 to 1 convertible to dimensional values by multiplying the Cartesian coordinate values of X and Y by a chord length of the airfoil. The upper surface and the lower surface form an enclosed airfoil shape. The aircraft is a supersonic aircraft, and the airfoil has a thickness-to-chord ratio of about 10%.


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    Titel :

    Airfoil for an aircraft for superior supersonic aerodynamic performance


    Beteiligte:

    Erscheinungsdatum :

    15.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRFOIL FOR SUPERSONIC AIRCRAFT

    O'LEARY PATRICK | Europäisches Patentamt | 2024

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    Aerodynamic forces on oscillating airfoil at supersonic speeds

    Miles, J.W. | Engineering Index Backfile | 1947