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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Hickey, D.H. (author) / Aoyagi, K. (author)


    Publication date :

    1960


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :