Stability of two-dimensional flow near a stagnation point in the presence of massive blowing

Abstract

is localized i. the center of the jet, for the axisymmetric case it occupies the entire transverse section of the jet.With increasing degree m = (Pe + B)/B of underexpansion (Pe is the pressure at the nozzle exit) the splitting region is shifted toward the nozzle.In the critical regime (M e = I), the splitting begins almost immediately after the nozzle exit.