Laminar flow experiments were performed in an 8-foot transonic pressure tunnel which was modified in order to simulate the conditions of an infinite span yawed wing. A liner in the tunnel provided a flow field around the yawed airfoil. The results were evaluated using hot-wire and fluctuating pressure measurements. Data were obtained for root-mean-square fluctuations, their spectra, and various cross product terms.


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    Titel :

    Flow quality measurements for the Langley 8-foot transonic pressure tunnel LFC experiment


    Beteiligte:

    Erscheinungsdatum :

    01.01.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Flow quality measurements for the Langley 8-foot transonic pressure tunnel LFC experiment

    JONES, GREGORY / STAINBACK, P. / HARRIS, CHARLES et al. | AIAA | 1989



    The Langley 8-ft transonic pressure tunnel laminar-flow-control experiment

    Bobbitt, Percy J. / Harvey, William D. / Harris, Charles D. et al. | NTRS | 1992



    Langley annular transonic tunnel

    Habel, L.W. / Henderson, J. / Miller, M.F. | Engineering Index Backfile | 1952