Author(s): N. Rajaratnam; S. Wu

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Abstract: This paper presents the results of an experimental study on intersecting circular turbulent jets of unequal momentum fluxes for an angle of intersection equal to 60 degrees. The flow has been divided into two regions, region 1 extending from the nozzle to the intersection point and region 2 covering the field downstream of the intersection point. In both these regions, the velocity and pressure fields were measured and analyzed and correlated with the ratio of the jet velocities at the two nozzles.

DOI: https://doi.org/10.1080/00221689209498907

Year: 1992