

ON THE CONTROL OF 3D TURBULENT BOUNDARY LAYER SEPARATION USING LOCAL VOLUMETRIC AND SURFACE GAS HEATING
Shalaev V.I.
Moscow Institute of Physics and Technology (State University), Moscow, Russia
Citation:
Shalaev V.I. On the control of 3d turbulent boundary layer separation using local volumetric and surface gas heating / V.I. Shalaev // Modern Science: Researches, Ideas, Results, Technologies.  Dnepropetrovsk: SPIC "Triacon".  2013.  Iss. #1(12).  PP. 104  110

Keywords: 3D boundary layer; turbulent flow; local volumetric and surface heating; separation flow control 
Abstracts:
Management of individual wrapping of the aircraft by inﬂuencing the course with the help of different physical mechanisms to improve the aerodynamic performance is one of the most promising and developing areas of modern aerodynamics. This paper presents the results of theoretical and numerical modeling of the inﬂuence of an electric discharge on the separation of the threedimensional turbulent boundary layer on a thin cone. We also give estimates of separation control by local heating of the surface. The aim of this study is to control the asymmetry of the ﬂow that occurs spontaneously around the head of the aircraft of various types at a critical angle of attack. The results indicate that the electric discharge is more efﬁcient means of separation than the local surface heating. 
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