The goal in this effort is to analyze the baseline TCA concept at transonic and supersonic cruise, then apply the natural flow wing design concept to obtain multipoint performance improvements. Analyses are conducted with OVERFLOW, a Navier-Stokes code for overset grids, using PEGSUS to compute the interpolations between the overset grids.


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    Title :

    Analysis and Multipoint Design of the TCA Concept


    Contributors:


    Publication date :

    1999-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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