Trailing-edge data for boundary layer/near wake thickness parameters are given airfoils and flat plates. Reynolds number effects are examined as a function of model size, velocity and boundary-layer tripping. Reference comparisons are made with boundary-layer calculations using potential-flow modeling and a finite-difference method for laminar and boundary layers. Open wind-tunnel corrections to angle to attack and camber are incorporated into the potential-flow modeling. It was found that the open tunnel flow turbulence affects early boundary-layer transition for the higher velocities. The theory still 'brackets' the data allowing some assessment of boundary-layer transition behaviour.


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    Titel :

    Airfoil trailing-edge flow measurements


    Weitere Titelangaben:

    Stroemungsmessungen an der Hinterkante von Tragfluegeln


    Beteiligte:
    Brooks, T.F. (Autor:in) / Marcolini, M.A. (Autor:in) / Pope, D.S. (Autor:in)

    Erschienen in:

    AIAA Journal ; 24 , 8 ; 1245-1251


    Erscheinungsdatum :

    1986


    Format / Umfang :

    7 Seiten, 9 Bilder, 8 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Airfoil trailing-edge flow measurements

    BROOKS, T. F. / MARCOLINI, M. A. / POPE, D. S. | AIAA | 1986


    Airfoil trailing-edge flow measurements

    Brooks, T. F. / Marcolini, M. A. / Pope, D. S. | NTRS | 1986


    Divergent-Trailing-Edge Airfoil Flow

    Thompson, B.E. | Online Contents | 1996


    Divergent-trailing-edge airfoil flow

    Thompson, Brian E. / Lotz, Robert D. | AIAA | 1996


    "Measurements on a Divergent Trailing-Edge Airfoil"

    Lotz, R. D. / Thompson, B. E. / Chen, C. F. A. et al. | British Library Conference Proceedings | 1999