Numerical Study on Mixing Characteristics of Circular and Non-Circular Jets.
Abstract
The study of non-circular jet flows has become important due to their various applications, such as aircraft exhaust, combustion chambers and injectors. The present paper examines the impact of elliptical, square, and triangular-shaped orifices on the mixing characteristics of a free jet with Mach number 0.8. Numerical simulations using an SST K-1 two-equation turbulence model were conducted with a Reynolds number of 3.46×105 for all cases. The mean velocity, decay rate, half-velocity width, spread rate, and turbulence intensity of the jet were analysed. The results showed that the triangular orifice provided the best mixing efficiency, with a shorter jet core length. The decay rate was found to be lowest for the square jet and highest for the triangular jet, which matches the previous research. The asymmetric jets experienced two axis-switching points, while the square jet experienced a 450 rotation of its axes but no axis-switching. The core region had lower turbulence levels, while the highest turbulence levels were in the shear layer.
Subjects
MACH number; JETS (Fluid dynamics); COMBUSTION chambers; REYNOLDS number; TURBULENCE
Description
Indexed in scopushttps://openurl.ebsco.com/EPDB%3Agcd%3A13%3A28280861/detailv2?sid=ebsco%3Aplink%3Aresult-item&id=ebsco%3Adoi%3A10.14429%2Fdsj.74.19626&bquery=Defence%20Science%20Journal&page=2&link_origin=www.google.com |
Article metrics10.31763/DSJ.v5i1.1674 Abstract views : | PDF views : |
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Conflict of interest
“Authors state no conflict of interest”
Funding Information
This research received no external funding or grants
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Peer review under responsibility of Defence Science Journal
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Acknowledgements:
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