Problem of drag as it affects short-field capability of aircraft; control of boundary layer by suction through distributed perforation; means for perforating doped fabric, and for drilling holes in metal or plywood; examples of geometric boundary layer control in Army L-17 Navion and Army YL-23 Twin Bonanza aircrafts; suction boundary control in Schweizer TG-3A sailplane with suction high lift system.


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    Title :

    Flow control by suction through distributed perforations


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1957 Drag



    Publication date :

    1957


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    FLOW CONTROL BY SUCTION THROUGH DISTRIBUTED PERFORATIONS

    CORNISH, JOSEPH J. | SAE Technical Papers | 1957



    Current tests on laminar-boundary-layer control by suction through perforations

    Butler, S. F. J. / Großbritannien, Aeronautical Research Council | TIBKAT | 1957