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Browsing by Subject "LEADING EDGE ROTATING, CYLINDER, PERFORMANCE, SYMMETRIC AEROFOIL"
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STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL (DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST), 2017-02)This research dealt with moving surface boundary layer control, applied to NACA 0018 aerofoil both by simulation and experiment. The moving surface was provided by a rotating cylinder placed at the leading edge of the ...
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