An experiment was performed on a low-aspect ratio wing to define the limits of the validity of codes which are used to predict the flow over modern fighter configurations. The focus of the experiment is to provide data at or near the true operating conditions of transonic aircraft. The Reynolds numbers reached in this experiment reproduce those experienced by an aircraft with a 5-m root chord, flying at 14 to 16 km, from Mach 0.6 to 0.8. The angle-of-attack range of the experiment extends into the regime of leading-edge separation.


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    Titel :

    Low aspect ratio wing code validation experiment


    Beteiligte:

    Erscheinungsdatum :

    01.01.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Low aspect ratio wing code validation experiment

    Olsen, M.E. / Seegmiller, H.L. | Tema Archiv | 1993


    Low aspect ratio wing code validation experiment

    Olsen, Michael E. / Seegmiller, H. L. | NTRS | 1993


    Low aspect ratio wing code validation experiment

    OLSEN, MICHAEL E. / SEEGMILLER, H. L. | AIAA | 1992


    Low Aspect Ratio Wing Code Validation Experiment

    Olsen, M.E. | Online Contents | 1993


    Low aspect ratio wing code validation experiment

    OLSEN, MICHAEL / SEEGMILLER, H. | AIAA | 1992