Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    AIAA-2002-5408 Multidisciplinary Design Optimization of Supersonic Fighter Wing Using Response Surface Methodology



    Conference:

    Symposium; 9th, Multidisciplinary analysis and optimization ; 2002 ; Atlanta, GA



    Publication date :

    2002-01-01


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English