Boundary layer control affects performance and structure of aircraft to such extent that it has to be considered in preliminary design of vehicle; factors to be included in parametric studies; primitive design method suggested is explained for case of subsonic STOL transport; high lift BLC systems and correlations of available data; state of art suggests flexible concept of multiple cell system.


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    Title :

    Design considerations for BLC STOL airplanes


    Additional title:

    Aero/Space Eng


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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