It is shown that in consideration of aircraft equipped with turbo-unit, necessity for providing air intake for turbine can be turned to advantage by arranging intake inlet to exert influence on boundary layer air flow; inherently applicable to jet propelled aircraft.


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    Title :

    Boundary layer control


    Additional title:

    Flight


    Published in:

    Flight ; 45 , n 1837


    Publication date :

    1944


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Boundary layer control

    Engineering Index Backfile | 1951


    Boundary layer control

    Lachmann, G.V. | Engineering Index Backfile | 1955


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