A simple approach for optimizing the jig-shape is proposed in this study. This simple approach is based on an unconstrained optimization problem and applied to a low-boom supersonic aircraft. In this study, the jig-shape optimization is performed using the two-step approach. First, starting design variables are computed using the least squares surface fitting technique. Next, the jig-shape is further tuned using a numerical optimization procedure based on in-house object-oriented optimization tool.


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    Title :

    Jig-Shape Optimization of a Low-Boom Supersonic Aircraft


    Contributors:

    Published in:

    Publication date :

    2018-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English