The streamlined blending proficiency of a circular sonic fly stream with an impact on a crosscable is considered computationally and tentatively at various scope of spout pressure proportion with the various directions along with the minor hub at the outlet. The crosswire in various direction is evident to lessen the quality of the stun wave development. Because of the nearness of wire, the pitot pressure swaying is decreased quick, which debilitates the stun cell structure. At the point where the crosscable is positioned at the focus , we see higher blending along with the significant hub. So also, once the crosswire is set at about ¼th and ¾th position, high blending advancement along with minor pivot is evident. It simultaneously demonstrates, as the situation of the crosscable diminished along with minor hub, there will be an increment in the blending proportion. Notwithstanding that we additionally found that, stream spread is high in significant hub contrasted with minor pivot because of the bifurcation of fly along upstream.