Two specially designed convex/concave profiles were tested in 0.75 x 0.42 mm UTAD-2 wind tunnel in National Aviation University of Ukraine at Reynolds numbers ranged from1.5 to 3.5x105 with the aim to estab-lish the feasibility and effectiveness of aerodynamic characteristics control using streamwise vortices, generated in boundary layer. The design of test models is presented together with test procedure, data acquisition system, and data reduction methodology.

The World Congress "Aviation in the X X I-st Century", 14-16 september [Текст] = Матеріали Всесвітнього конгресу "Авіація ХХІ століття" 14-16 вересня 2003 року / International Civil Aviation Organization; Ministry of Education and Science of Ukraine; National Academy of Sciences of Ukraine; National Aviation University. — Kyiv : NAU, 2003. — 438 p. : il.