Typical 4-engine jet has wing of aspect ratio 7; 3-component longitudinal force and moment data and boundary layer flow requirements are presented and results analyzed in terms of estimated take-off and landing performance; effect on performance of source of boundary-layer-control airflow is considered.


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    Titel :

    Large-scale wind-tunnel tests and evaluation of low-speed performance of 35° sweptback wing jet transport model equipped with blowing boundary-layer-control flap and leading-edge slat


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Hickey, D.H. (Autor:in) / Aoyagi, K. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    52 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :