A Reynolds-average Navier Stokes method developed for rotorcraft type of flow problems is applied for predicting the forces and moments of forebody models at high-angle-of-attack dynamic conditions and for providing insight into the flow characteristics at these conditions. Wind-tunnel results from rotary testing on generic forebody models conducted by NASA Langley and DERA are used for comparison. This paper focuses on the steady-state flow problem.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Prediction of Flows about Forebodies at High-Angle-of-Attack Dynamic Conditions


    Beteiligte:
    vanDam, C. P. (Autor:in) / Saephan, S. (Autor:in) / Fremaux, C. M. (Autor:in) / DalBello, T. (Autor:in)


    Erscheinungsdatum :

    01.03.2003


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch