Experimental and numerical study on low-temperature supersonic ejector

Ejectors have emerged as a viable solution for handling Boil-Off-Gas (BOG) generated by cryogenic storage tanks. The efficiency of ejector-based systems plays is highly dependent on the ejector's performance which is influenced by various factors including the geometry of the ejector and the bo...

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Main Authors: Hadi Samsam-Khayani, Sang Youl Yoon, Mirae Kim, Kyung Chun Kim
Format: Article
Language:English
Published: Elsevier 2023-11-01
Series:International Journal of Thermofluids
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2666202723001246
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author Hadi Samsam-Khayani
Sang Youl Yoon
Mirae Kim
Kyung Chun Kim
author_facet Hadi Samsam-Khayani
Sang Youl Yoon
Mirae Kim
Kyung Chun Kim
author_sort Hadi Samsam-Khayani
collection DOAJ
description Ejectors have emerged as a viable solution for handling Boil-Off-Gas (BOG) generated by cryogenic storage tanks. The efficiency of ejector-based systems plays is highly dependent on the ejector's performance which is influenced by various factors including the geometry of the ejector and the boundary conditions. In this study, an axisymmetric supersonic ejector was designed, optimized, and evaluated for BOG removal. The baseline geometric dimensions design of the ejector was obtained via theoretical analysis. Subsequently, computational fluid dynamics (CFD) simulations were employed to optimize the boundary conditions and geometrical parameters. Experimental investigations were conducted to validate the design and evaluate the ejector's performance. The results highlighted the significant influence of two key parameters, namely, the mixing chamber diameter (Dm) and the nozzle exit position (NXP), on the ejector's performance. Optimized Dm showed an increase of about 12.5% compared with the baseline geometry. By operating the ejector within its on-design geometric and boundary conditions, the maximum entrainment ratio (ER) was achieved. The CFD models successfully identified and validated various flow phenomena, including double choke, single choke, and backflow, which were consistent with the experimental observations. Both the numerical models and experimental findings demonstrated that the modified ejector achieved an entrainment ratio of 1.06 under its design condition showing a 33.66% increase compared with that obtained using the baseline geometry. These results indicate the potential of the supersonic ejector as an alternative solution for BOG applications, emphasizing its efficacy in handling this industrial challenge.
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spelling doaj.art-32e8074b428f47ce8fb19806d9ad7a4a2023-12-07T05:30:39ZengElsevierInternational Journal of Thermofluids2666-20272023-11-0120100407Experimental and numerical study on low-temperature supersonic ejectorHadi Samsam-Khayani0Sang Youl Yoon1Mirae Kim2Kyung Chun Kim3School of Mechanical Engineering, Eco-friendly Smart Ship Parts Technology Innovation Center, Pusan National University, Busan, 46241, South KoreaRolls-Royce and Pusan National University Technology Centre, Pusan National University, Busan, 46241, South KoreaRolls-Royce and Pusan National University Technology Centre, Pusan National University, Busan, 46241, South KoreaSchool of Mechanical Engineering, Eco-friendly Smart Ship Parts Technology Innovation Center, Pusan National University, Busan, 46241, South Korea; Corresponding author.Ejectors have emerged as a viable solution for handling Boil-Off-Gas (BOG) generated by cryogenic storage tanks. The efficiency of ejector-based systems plays is highly dependent on the ejector's performance which is influenced by various factors including the geometry of the ejector and the boundary conditions. In this study, an axisymmetric supersonic ejector was designed, optimized, and evaluated for BOG removal. The baseline geometric dimensions design of the ejector was obtained via theoretical analysis. Subsequently, computational fluid dynamics (CFD) simulations were employed to optimize the boundary conditions and geometrical parameters. Experimental investigations were conducted to validate the design and evaluate the ejector's performance. The results highlighted the significant influence of two key parameters, namely, the mixing chamber diameter (Dm) and the nozzle exit position (NXP), on the ejector's performance. Optimized Dm showed an increase of about 12.5% compared with the baseline geometry. By operating the ejector within its on-design geometric and boundary conditions, the maximum entrainment ratio (ER) was achieved. The CFD models successfully identified and validated various flow phenomena, including double choke, single choke, and backflow, which were consistent with the experimental observations. Both the numerical models and experimental findings demonstrated that the modified ejector achieved an entrainment ratio of 1.06 under its design condition showing a 33.66% increase compared with that obtained using the baseline geometry. These results indicate the potential of the supersonic ejector as an alternative solution for BOG applications, emphasizing its efficacy in handling this industrial challenge.http://www.sciencedirect.com/science/article/pii/S2666202723001246Supersonic ejectorBoil off gasOptimizationCryogenic temperatureCFD
spellingShingle Hadi Samsam-Khayani
Sang Youl Yoon
Mirae Kim
Kyung Chun Kim
Experimental and numerical study on low-temperature supersonic ejector
International Journal of Thermofluids
Supersonic ejector
Boil off gas
Optimization
Cryogenic temperature
CFD
title Experimental and numerical study on low-temperature supersonic ejector
title_full Experimental and numerical study on low-temperature supersonic ejector
title_fullStr Experimental and numerical study on low-temperature supersonic ejector
title_full_unstemmed Experimental and numerical study on low-temperature supersonic ejector
title_short Experimental and numerical study on low-temperature supersonic ejector
title_sort experimental and numerical study on low temperature supersonic ejector
topic Supersonic ejector
Boil off gas
Optimization
Cryogenic temperature
CFD
url http://www.sciencedirect.com/science/article/pii/S2666202723001246
work_keys_str_mv AT hadisamsamkhayani experimentalandnumericalstudyonlowtemperaturesupersonicejector
AT sangyoulyoon experimentalandnumericalstudyonlowtemperaturesupersonicejector
AT miraekim experimentalandnumericalstudyonlowtemperaturesupersonicejector
AT kyungchunkim experimentalandnumericalstudyonlowtemperaturesupersonicejector