This article deals with the design of helicopter UAV airframe components. There is a description of UAV airframe design modelling involving already existing components in three-dimensional (3D) form. The modelling methodology focuses in detail on proposed bulkheads by using “top-downbottom-up” methodology. In conclusion, there is a brief description of all proposed bulkheads and an outline of possible solutions for how to design airframe stringers.


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    Title :

    HELICOPTER UAV FUSELAGE BULKHEAD MODELLING


    Contributors:


    Publication date :

    2016




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




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