27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-3.2.1

WIND TUNNEL INVESTIGATION FOR OSCILLATORY BLOWING ON HIGH LIFT SYSTEMS

C. Nae
INCAS, Romania

Keywords: active flow control, high lift systems, wind tunnel testing

Results from wind tunnel investigation for high lift system with oscillatory blowing are presented for 2D and 2.5D configurations. Various flap settings and blowing system characteristics have been tested in order to evaluate oscillatory blowing for active high lift system. System efficiency and practical limitations are presented.

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