Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen

Liquid nitrogen is a widely utilized effective low-temperature cooling medium, also employed in the ATR-GG (Gas Generator cycle Air Turbo rocket) engine to cool high-temperature components. Due to the high-temperature work environment and the ease with which liquid nitrogen evaporates and boils, liquid nitrogen would experience a flash boiling process. In order to study the influence of flash boiling on spray characteristics, experiments and simulations were conducted with two types of hollow-cone nozzles and two types of solid-cone nozzles under subcooled water at normal temperature which is not affect by flash boiling and superheat liquid nitrogen inflow conditions. The research found that flashing already begins inside the nozzle, significantly reducing the discharge coefficient of the solid-cone nozzle. The nitrogen gas-liquid mixture fills the air core of the hollow-cone spray, resulting in a comparatively smaller impact on the discharge coefficient. The liquid nitrogen spray exhibit spray collapse, unable to achieve the spray cone angels as the water spray. The major reason is that during the flashing process, nitrogen vapor expansion enhances the axial velocity, reducing the spray cone angle. The study recommends using hollow-cone nozzles to mitigate the impact of flash boiling on the spray characteristics.

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Publication Details

Journal
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Published
2024-08-21
DOI
https://doi.org/10.1177/09544100241275251
Citations
1
Primary Topic
Fluid Dynamics and Heat Transfer
Type
article
Field-Weighted Citation Impact
0.37
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article

Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen

Binglong Zhang, Qingjun Zhao, Bin Hu, Yihong Lu et al.
1 citations
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Fluid Dynamics and Heat Transfer
0.37
article

Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen

Binglong Zhang, Qingjun Zhao, Bin Hu, Yihong Lu, Wei Zhao, Xuesen Yang
article en
1 citations

Abstract

Liquid nitrogen is a widely utilized effective low-temperature cooling medium, also employed in the ATR-GG (Gas Generator cycle Air Turbo rocket) engine to cool high-temperature components. Due to the high-temperature work environment and the ease with which liquid nitrogen evaporates and boils, liquid nitrogen would experience a flash boiling process. In order to study the influence of flash boiling on spray characteristics, experiments and simulations were conducted with two types of hollow-cone nozzles and two types of solid-cone nozzles under subcooled water at normal temperature which is not affect by flash boiling and superheat liquid nitrogen inflow conditions. The research found that flashing already begins inside the nozzle, significantly reducing the discharge coefficient of the solid-cone nozzle. The nitrogen gas-liquid mixture fills the air core of the hollow-cone spray, resulting in a comparatively smaller impact on the discharge coefficient. The liquid nitrogen spray exhibit spray collapse, unable to achieve the spray cone angels as the water spray. The major reason is that during the flashing process, nitrogen vapor expansion enhances the axial velocity, reducing the spray cone angle. The study recommends using hollow-cone nozzles to mitigate the impact of flash boiling on the spray characteristics.

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace EngineeringVol. 238(15)
Chinese Academy of Sciences (CN), Institute of Engineering Thermophysics (CN), University of Chinese Academy of Sciences (CN)
Openalex Percentile: Top 44%
Fluid Dynamics and Heat Transfer
0.37
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Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen — Binglong Zhang, Qingjun Zhao, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering (2024) | TGRS Research Map | TGRS