Evolution of successful distributed suction boundary layer control systems at Mississippi State University is described; analysis of various high-lift aircraft has been performed to determine wing lift and increment of lift due to boundary layer control; operational problems of distributed suction boundary layer control aircraft and comparison with other means of achieving similar lift coefficients are presented. (06626)


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    Title :

    Distributed suction boundary layer control for high lift


    Additional title:

    SAE Paper


    Contributors:

    Conference:

    SAE Meeting ; 1968 Boundary layer


    Published in:

    Publication date :

    1968


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :