1. Aeroelastic tailoring with tow-steered composites 2. Aeroelastic tailoring with functionally-graded metals 3. Wing box topology optimization - Curvilinear rib/spar/stiffener placement - Cellular-based stringer topologies - Optimal topology of lightening holes within ribs/spars - 3D level set methods


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    Title :

    Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch


    Contributors:

    Conference:

    The Technical Cooperating Program Technical Panel 4 (TTCP TP-4) Annual Meeting ; 2014 ; Ottawa, CA


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




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