Results of investigation designed to study how pilots use high lift available with blowing boundary-layer-control leading- and trailing-edge flaps to provide operation experience, and to determine limiting factors in choice of landing approach speed when wing stall is delayed to high angles of attack.


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    Titel :

    Flight investigation of low-speed characteristics of 45° swept-wing fighter-type airplane with blowing boundary-layer control applied to leading- and trailing-edge flaps


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Quigley, H.C. (Autor:in) / Anderson, S.B. (Autor:in) / Innis, R.C. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    44 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :