This current work evaluates the efficacy of a co-flow nozzle for cold spray applications with
the aim of mitigating nozzle clogging issues, which can occur during long-duration …

Abstract Effect of an annular co-flow jet on the center jet at subsonic, correctly expanded and
underexpanded sonic conditions was studied experimentally. It is found that the co-flow …

This paper presents the experimental results of subsonic and underexpanded sonic jets
delivered from a central nozzle surrounded by a co-flow. The role of central nozzle lip …

A detailed experimental study was carried out to investigate the behaviour of a Mach 2
primary jet in the presence of a Mach 1.6 annular co-flow. The lip thickness of the inner …

This paper presents the results of high-speed co-flow jets from orifices with two annular gaps
tested with a single feed system. The co-flow models consist of a primary orifice of 10 mm …

Purpose This study aims to present the numerical study on supersonic jet mixing
characteristics of the co-flow jet by varying lip thickness (LT). The LT chosen for the study is …

This paper presents the experimental results of underexpanded jets delivered from a central
nozzle surrounded by a co-flow. The co-flow is found to be effective in elongating the …

Purpose The purpose of this study is to understand experimentally the mixing characteristics
of a two-stream exhaust system with a supersonic Mach 1.5 primary jet that exits the …

The mixing characteristics of a Mach 1.9 jet at three levels of overexpansion, corresponding
to nozzle pressure ratio (NPR) 3, 4 and 5, in the presence of a sonic co-flow (secondary …

Purpose In comparison to a nozzle with a larger/finite separation distance (Thanigaiarasu et
al., 2019), a thin-lip nozzle (Srinivasarao et al., 2017) minimizes drag. Coaxial nozzles with …