An effective method of designing low drag, attached flow automobile forebodies has been developed. Based on a potential flow panel method, a series of computer programs is used to define idealized pressure gradients at several forward corner locations including the hood, fender, windshield header and A-pillar. Idealized pressure gradients for several radii at each corner location are analyzed using a turbulent boundary layer separation criterion to determine if real-world viscous flow will remain attached. Correlation with wind tunnel test results is included. A non-circular, attached flow hood corner shape is developed based on the separation criterion and an inverse (geometry defining) computer method.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analysis and design of automobile forebodies using potential flow theory and a boundary layer separation criterion


    Weitere Titelangaben:

    Untersuchung und Entwurf der Vorderteile von Kraftfahrzeugen mit Hilfe der Potentialstroemungstheorie und einem Grenzschichttrennungskriterium


    Beteiligte:
    Paul, J.C. (Autor:in) / LaFond, J.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    21 Seiten, 34 Bilder, 25 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Analysis and Design of Automobile Forebodies Using Potential Flow Theory and a Boundary Layer Separation Criterion

    Paul,J.C. / LaFond,J.G. / Airflow Sciences Corp.,US et al. | Kraftfahrwesen | 1983



    Inlet Boundary-Layer Shapes on Four Aircraft Forebodies at Mach 6

    Pierce L. Lawing / Charles B. Johnson | AIAA | 1978



    Inlet boundary-layer shapes on four aircraft forebodies at Mach 6

    Lawing, P. L. / Johnson, C. B. | NTRS | 1978