Abstract An Airplane model design without a vertical stabilizer comprising, a fuselage, twisted wings and horizontal stabilizer, wherein, said fuselage is connected with the twisted wings and the horizontal stabilizer; said horizontal stabilizer having an elevator, and a power system for thrust and controlling; characterized in that, the twisted wings made up of airfoil that is twisted in a negative angle wherein twist increases towards the extreme end of the wing, away from the fuselage so as to provide balancing of the adverse yaw. Application No: Applicant Name: (1) Abhishek S. Pawar (2) Atharva Mahajan (3) Vrushal Modake (4) Ashish Dharme Total No of Sheets: 05 Page 4 of 5 Figure 4 Sectional View of the wing of the airplane without vertical tail assembly (1) Abhishek S. Pawar (2) Atharva Mahajan (3) Vrushal Modake (4) Ashish Dharme Applicant Applicant Applicant Applicant


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    Titel :

    AN AIRPLANE DESIGN STUCTURE WITHOUT VERTICAL STABILIZER


    Beteiligte:
    PAWAR ABHISHEK S (Autor:in) / MAHAJAN ATHARVA (Autor:in) / MODAKE VRUSHAL (Autor:in) / DHARME ASHISH (Autor:in) / SHERJE NITIN P (Autor:in)

    Erscheinungsdatum :

    08.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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