In this work, a previously developed mean flow boundary condition will be validated for unsteady flows. The test cases will be several reference benchmark flows consisting of vortical gusts convecting in a uniform mean flow, as well as the more realistic case of a vortical gust impinging on a loaded 2D cascade. The results will verify that the mean flow boundary condition both imposes the desired mean flow as well as having little or no effect on the instantaneous unsteady solution.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Unsteady Validation of a Mean Flow Boundary Condition for Computational Aeroacoustics


    Beteiligte:
    Hixon, R. (Autor:in) / Zhen, F. (Autor:in) / Nallasamy, M. (Autor:in) / Sawyer, S> (Autor:in) / Dyson, R. (Autor:in)

    Kongress:

    42nd AIAA Aerospace Sciences Meeting ; 2004 ; Reno, NV, United States


    Erscheinungsdatum :

    2004-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :