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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    Titel :

    Jig-Shape Optimization of a Low-Boom Supersonic Aircraft


    Beteiligte:
    Pak, Chan-gi (Autor:in)

    Kongress:

    AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; 2018 ; Kissimmee, FL, United States
    AIAA SciTech 2018 ; 2018 ; Kissimmee, FL, United States


    Erscheinungsdatum :

    08.01.2018


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch