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.
Prandtl, Uø ber flussigkeitsbewegung mit kleiner reibung, Verhandlungen des III
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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.