Because of importance of internal losses in slot and ducts, attempt was made to develop satisfactory internal systems, after which wing was tested in Lockheed wind tunnel with suction applied; series of tests made at full scale and high Reynolds numbers in flight applying boundary layer control to envelop that had been employed in low drag airfoil investigation.


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    Titel :

    Flight and tunnel test research on boundary-layer control


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1949


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Boundary layer transition flight test observations

    BERKOWITZ, A. / KYRISS, C. / MARTELLUCCI, A. | AIAA | 1977


    Flight and wind-tunnel investigations on boundary-layer transition

    HORSTMANN, K. H. / QUAST, A. / REDEKER, G. | AIAA | 1990




    Shuttle orbiter boundary layer transition at flight and wind tunnel conditions

    Goodrich, W. D. / Derry, S. M. / Bertin, J. J. | NTRS | 1983