Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack



    Conference:

    INTERNATIONAL CONGRESS; 22nd, International Council of the Aeronautical Sciences ; 2000 ; Harrogate



    Publication date :

    2000-01-01


    Size :

    2.5.2


    Remarks:

    HELD ON CD-ROM



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English