Uniform suction and blowing eliminate separation on a NACA4412 wing at 11 degrees angle of attack and increase lift up to 11.5 percent, but drag increases enough to reduce aerodynamic efficiency.
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Separation control applied to the turbulent flow around a NACA4412 wing section
Uniform suction and blowing eliminate separation on a NACA4412 wing at 11 degrees angle of attack and increase lift up to 11.5 percent, but drag increases enough to reduce aerodynamic efficiency.