The present lift generating fuselage (1) for aircraft mainly comprises of: a novel aerofoil shaped fuselage (1A); or a novel aerofoil shaped fuselage body (2); and integral webs (3); or a novel aerofoil shaped fuselage body (2); integral webs (3) and overhead central wing (4).


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    Title :

    LIFT GENERATING FUSELAGE FOR AIRCRAFT


    Contributors:

    Publication date :

    2018-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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