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    Title :

    1135-1205 Aerodynamic Optimization of Supersonic Wing-Nacelle Configuration Using an Adjoint Method with the Unstructured-Grid Approach



    Conference:

    International workshop; 2nd, Numerical simulation technology for design of next generation supersonic civil transport ; 2000 ; Tokyo



    Publication date :

    2000-01-01


    Size :

    10 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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