The present invention refers to aircraft tail surfaces and more particularly to a configuration of an aircraft tail surface (1) with a single protrusion (3) for improving air flow control with no or negligible drag penalty.


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    Title :

    AIRCRAFT TAIL SURFACE


    Additional title:

    FLUGZEUGHECKFLÄCHE
    SURFACE ARRIÈRE D'AÉRONEF


    Contributors:

    Publication date :

    2025-05-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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