Experiments on laminar suction wings at Institute for Aerodynamics, Zurich, verified full chord laminar flow and low wing profile drags by means of suction up to Re 2.5×106 wing chord; to investigate behavior at reduced turbulence level, corresponding to flight conditions, 15%-thick slotted low drag suction wing model was tested in Langley Field TDT tunnel; for comparison, Zurich BLC results and profile drags of various non-suction wings are presented with laminar and turbulent friction drag of flat plates.


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    Titel :

    Recent developments in field of low drag boundary layer suction research


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Pfenninger, W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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