“…Moreover, it can be implemented with the minimum penalty of the aircraft observability. 3 Because of these advantages, several approaches to fluidic thrust-vectoring have been proposed in the past years, including Coanda effect by use of coflow blowing and counter-flow aspiration 4,5 shock vector control, [6][7][8][9][10] throat-skewing 11 and Dual-Throat Nozzle (DTN) configuration. 2,12,13 Among these, the DTN configuration has shown to achieve greater thrust vectoring efficiency, without compromising the axial component of thrust.…”