In this paper the capabilities of an automated CFD system which is currently available at NLR are demonstrated. Transonic flow around the AS28G wing/body configuration and hypersonic flow through a generic three-dimensional mixed-compression airbreathing inlet are simulated. An assessment of the level of automation of the current CFD-system is made. The problem-turnaround time lies within the order of a week for both applications.


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    Titel :

    Demonstration of an Automated CFD System for Three-Dimensional Flow Simulations


    Beteiligte:
    J. W. Vanderburg (Autor:in) / J. E. J. Maseland (Autor:in) / R. Hagmeijer (Autor:in) / K. M. J. Decock (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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