The invention relates to an aerodynamic body for flying objects having a hybrid laminar flow control, wherein the aerodynamic body comprises:- a load bearing supporting structure (11) having at least one hollow chamber forming a low-pressure suction plenum (18);- a perforated panel skin (20) arranged on the supporting structure of the aerodynamic body having an outer surface (23), the perforated panel skin has a plurality of openings being in fluid communication with the low-pressure suction plenum; and- at least one compressor (40) having at least one inlet (41) and at least one outlet (42);characterized in that- the compressor is located inside the hollow chamber; and- the inlet of the compressor protrudes into the low-pressure suction plenum and the outlet sticks out of the low-pressure suction plenum into an ambient pressure compartment so that a low-pressure within the low-pressure suction plenum established by the compressor results in air suction through the openings of the perforated panel skin.


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    Title :

    AERODYNAMIC BODY FOR FLYING OBJECTS


    Additional title:

    AERODYNAMISCHER KÖRPER FÜR FLUGOBJEKTE
    CORPS AÉRODYNAMIQUE POUR DES OBJETS VOLANTS



    Publication date :

    2022-11-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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