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  1. MJOGRADY25

    Enhancement of laminar flow across an airfoil by PLFC

    SEPARATION/DESTRUCTION OF THE BOUNDRY LAYER AT LOW SPEEDS AND HIGH ANGLE OF ATTACK CAN BE INHIBITED AND DELAYED BY SEVERAL TECHNIQUES. ONE OF THESE IS VACUUM-INDUCED FLOW THROUGH THE PERFORATED SURFACE OF THE AIRFOIL WING.--ironicly called '\" positive laminar flow control" THIS WAS...
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