Rotating co-flow jets with horizontal lip and shape transition

Abstract

Purpose

Control over large-scale coherent structures and stream-wise vortices lead to enhanced entrainment/conservation of the jet which is desirable for most free jet applications such as design of combustion chamber in jet engines and flame length elongation of welding torch used for metal cutting.

Design/methodology/approach

A co-flow nozzle with lip thickness of 2 mm, between the primary (inner) and secondary (outer) flow, is selected. Three nozzle combinations are used, i.e. C–C (circle–circle), C–E (circle–ellipse) and C–S (circle–square) for acquiring comparative data. For these nozzle combinations, inner nozzle exit plane is kept as a circle, whereas the outer nozzle exit planes are varied to circle, ellipse and square. The exit plane area of outer nozzle for the nozzle combinations has equivalent diameter, D_e. The nozzles are fabricated in a way that the outer nozzle can be rotated along the longitudinal axis, keeping the inner nozzle intact.

Findings

The C–C nozzle combination is effective in low Mach number regime in decaying the jet, when the rotational component is introduced. Around 30% reduction in the jet core length is observed for the C–C nozzle combinations without any lip. The C–E nozzle shows sedative result in decaying or preserving the jet. The C–S nozzle combination shows interesting phenomenon, whereby the low subsonic case tends to conserve the jet by 15% and the higher subsonic case tends to decay the jet by 10%.

Originality/value

The developed nozzle systems show both conservative and destructive effect on the jet, which is desirable for the mentioned applications.

Citation

S.A., D.P., Thanigaiarasu, S. and Premanand, N. (2021), "Rotating co-flow jets with horizontal lip and shape transition", Aircraft Engineering and Aerospace Technology, Vol. 93 No. 10, pp. 1681-1690. https://doi.org/10.1108/AEAT-05-2020-0095