27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-3.7.2

APPLICATION OF TANGENTIAL JET BLOWING FOR SUPPRESSION OF SHOCK-INDUCED FLOW SEPARATION AT TRANSONIC SPEEDS

A. V. Petrov, V. D. Bokser, G. G. Sudakov, P. V. Savin
TsAGI, Russian Federation

Keywords: aerodynamic characteristics, wing, shock-induced flow separation, tangential jet blowing

The results of calculation and experimental investigations of efficiency of application of compressed air jet tangential blowing through a slot nozzle over upper surface of a supercritical swept wings for suppression of shock-induced boundary layer separation at a high transonic speeds are presented

view full paper