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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    Title :

    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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :