A broad program to develop advanced, reliable, and user oriented three-dimensional viscous design techniques for supersonic inlet systems, and encourage their transfer into the general user community is discussed. Features of the program include: (1) develop effective methods of computing three-dimensional flows within a zonal modeling methodology; (2) ensure reasonable agreement between said analysis and selective sets of benchmark validation data; (3) develop user orientation into said analysis; and (4) explore and develop advanced numerical methodology.


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    Titel :

    Three-dimensional viscous design methodology for advanced technology aircraft supersonic inlet systems


    Beteiligte:

    Kongress:

    Aerospace Sci. Meeting ; 1984 ; Reno, NV, United States


    Erscheinungsdatum :

    01.12.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch