The optimum nozzle exit position and the behaviour of a turbulent flow in an ejector designed for natural draft burner

This study investigated the near and far stream behaviour of a turbulent flow through an ejector at different axial positions of the nozzle. The study was conducted numerically for a throat-to-nozzle exit axial distance of 5 mm-20 mm. The secondary to the primary stream velocity ratio and the magnitude of the boundary layer fluctuation at the nozzle exit increased with the reducing axial distance. The potential core decayed as the flow approached a critical Reynolds number, and the increase in boundary layer fluctuation suppressed the near stream turbulence and momentum transfer by turbulent eddies. The model of the core length as a function of the throat-to-nozzle exit distance revealed a linear profile. Two models described the species concentration along the jet axis as a function of the root mean squared value of the fluctuating velocity because the flow behaved differently near and far streams due to the different controlling mechanisms.

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Publication Details

Journal
Progress in Computational Fluid Dynamics An International Journal
Published
2025-01-01
DOI
https://doi.org/10.1504/pcfd.2025.143737
Citations
1
Primary Topic
Refrigeration and Air Conditioning Technologies
Type
article
Field-Weighted Citation Impact
0.71
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article

The optimum nozzle exit position and the behaviour of a turbulent flow in an ejector designed for natural draft burner

Godswill N. Nwaji, H. O. Okoro, O. C. Nwufo, E.E. Anyanwu et al.
1 citations
Progress in Computational Fluid Dynamics An International Journal
Refrigeration and Air Conditioning Technologies
0.71
article

The optimum nozzle exit position and the behaviour of a turbulent flow in an ejector designed for natural draft burner

Godswill N. Nwaji, H. O. Okoro, O. C. Nwufo, E.E. Anyanwu, Chukwunonso F. Nwoye, C. A. Okoronkwo
article en
1 citations

Abstract

This study investigated the near and far stream behaviour of a turbulent flow through an ejector at different axial positions of the nozzle. The study was conducted numerically for a throat-to-nozzle exit axial distance of 5 mm-20 mm. The secondary to the primary stream velocity ratio and the magnitude of the boundary layer fluctuation at the nozzle exit increased with the reducing axial distance. The potential core decayed as the flow approached a critical Reynolds number, and the increase in boundary layer fluctuation suppressed the near stream turbulence and momentum transfer by turbulent eddies. The model of the core length as a function of the throat-to-nozzle exit distance revealed a linear profile. Two models described the species concentration along the jet axis as a function of the root mean squared value of the fluctuating velocity because the flow behaved differently near and far streams due to the different controlling mechanisms.

Progress in Computational Fluid Dynamics An International JournalVol. 25(1)
Federal University of Technology Owerri (NG), The Federal Polytechnic, Ado-Ekiti (NG)
Openalex Percentile: Top 37%
Refrigeration and Air Conditioning Technologies
0.71
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