High-resolution skin friction fields in separated flows over a 65° delta wing and a 76/40° double-delta wing with different junction fillets are obtained by using quantitative global skin friction diagnostics based on luminescent oil visualizations. The topological features such as separation and attachment lines on these delta wings are identified, and the effects of the pitch, yaw, and roll angles on the skin friction topology are studied systematically. The topological consistency of the measured skin friction fields on the delta wings is examined by using the Poincare-Bendixson index formula.


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    Titel :

    Effects of pitch, yaw, and roll on delta wing skin friction topology




    Erscheinungsdatum :

    2016



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    275/7040



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    Effects of Yaw and Roll Angles on Skin Friction Topology on Delta Wings

    Woodiga, Sudesh / Liu, Tianshu / Ramasamy, RS Vewen | AIAA | 2012


    Effects of Yaw and Roll Angles on Skin Friction Topology on Delta Wings

    Woodiga, S. / Liu, T. / Ramasamy, R.S.V. et al. | British Library Conference Proceedings | 2012


    The Predictability of Skin-Friction Line Topology on a Rolled Delta Wing

    Addington, G. / Nelson, R. / AIAA | British Library Conference Proceedings | 1998


    The predictability of skin-friction line topology on a rolled delta wing

    Addington, Gregory / Nelson, Robert | AIAA | 1998