Standard

Design and performance analysis of a Joule-Thomson cryocooler systems. / Tarish, Ali Lateef; Alwan, Naseer T.; Ali, Bashar M. и др.
в: Energy Reports, Том 11, 01.06.2024, стр. 4572-4586.

Результаты исследований: Вклад в журналСтатьяРецензирование

Harvard

Tarish, AL, Alwan, NT, Ali, BM, Ali, OM, Aslan, SR & Alomar, OR 2024, 'Design and performance analysis of a Joule-Thomson cryocooler systems', Energy Reports, Том. 11, стр. 4572-4586. https://doi.org/10.1016/j.egyr.2024.04.034

APA

Tarish, A. L., Alwan, N. T., Ali, B. M., Ali, O. M., Aslan, S. R., & Alomar, O. R. (2024). Design and performance analysis of a Joule-Thomson cryocooler systems. Energy Reports, 11, 4572-4586. https://doi.org/10.1016/j.egyr.2024.04.034

Vancouver

Tarish AL, Alwan NT, Ali BM, Ali OM, Aslan SR, Alomar OR. Design and performance analysis of a Joule-Thomson cryocooler systems. Energy Reports. 2024 июнь 1;11:4572-4586. doi: 10.1016/j.egyr.2024.04.034

Author

Tarish, Ali Lateef ; Alwan, Naseer T. ; Ali, Bashar M. и др. / Design and performance analysis of a Joule-Thomson cryocooler systems. в: Energy Reports. 2024 ; Том 11. стр. 4572-4586.

BibTeX

@article{4b954c98ea0045c591d3e05defc4aef5,
title = "Design and performance analysis of a Joule-Thomson cryocooler systems",
abstract = "The aim of the work is to develop a mathematical model which has capability to analyses the design parameters as a function of operations conditions for single and multi-stage Joule Thomson Cryocooler System JTCS. The operations conditions are inlet and outlet pressure, precooling temperature, and mass flow rate. The design parameters are expansion device (length, diameter, and Joule Thomson coefficient), heat exchanger (length, diameter, and effectiveness) and gas type (nitrogen, oxygen, and argon). Theoretical results for nitrogen, oxygen, and argon at initial pressure of 25 MPa, initial temperature of 20ºC, indicate that the final temperature equal to (-16.46ºC, −37.34ºC and −56.75ºC) respectively at single stage JTCS. It also shows the possibility of decreasing the final temperature to (-194ºC, −180.9ºC and −183.8ºC) respectively at multistage JTCS. The experimental rig has been constructed for satisfying mathematical model. The experimental results for nitrogen gas show a temperature drop of 6.5ºC when the initial pressure and temperature were 3 MPa and 20ºC respectively. Theoretical results were validated using experimental measurements on the other hand. The computer program has been built to carry out the analysis required for solving the parameters of JTCS under different operations conditions with good agreement compared to recent published researchers.",
author = "Tarish, {Ali Lateef} and Alwan, {Naseer T.} and Ali, {Bashar M.} and Ali, {Obed M.} and Aslan, {Sami R.} and Alomar, {Omar R.}",
year = "2024",
month = jun,
day = "1",
doi = "10.1016/j.egyr.2024.04.034",
language = "English",
volume = "11",
pages = "4572--4586",
journal = "Energy Reports",
issn = "2352-4847",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Design and performance analysis of a Joule-Thomson cryocooler systems

AU - Tarish, Ali Lateef

AU - Alwan, Naseer T.

AU - Ali, Bashar M.

AU - Ali, Obed M.

AU - Aslan, Sami R.

AU - Alomar, Omar R.

PY - 2024/6/1

Y1 - 2024/6/1

N2 - The aim of the work is to develop a mathematical model which has capability to analyses the design parameters as a function of operations conditions for single and multi-stage Joule Thomson Cryocooler System JTCS. The operations conditions are inlet and outlet pressure, precooling temperature, and mass flow rate. The design parameters are expansion device (length, diameter, and Joule Thomson coefficient), heat exchanger (length, diameter, and effectiveness) and gas type (nitrogen, oxygen, and argon). Theoretical results for nitrogen, oxygen, and argon at initial pressure of 25 MPa, initial temperature of 20ºC, indicate that the final temperature equal to (-16.46ºC, −37.34ºC and −56.75ºC) respectively at single stage JTCS. It also shows the possibility of decreasing the final temperature to (-194ºC, −180.9ºC and −183.8ºC) respectively at multistage JTCS. The experimental rig has been constructed for satisfying mathematical model. The experimental results for nitrogen gas show a temperature drop of 6.5ºC when the initial pressure and temperature were 3 MPa and 20ºC respectively. Theoretical results were validated using experimental measurements on the other hand. The computer program has been built to carry out the analysis required for solving the parameters of JTCS under different operations conditions with good agreement compared to recent published researchers.

AB - The aim of the work is to develop a mathematical model which has capability to analyses the design parameters as a function of operations conditions for single and multi-stage Joule Thomson Cryocooler System JTCS. The operations conditions are inlet and outlet pressure, precooling temperature, and mass flow rate. The design parameters are expansion device (length, diameter, and Joule Thomson coefficient), heat exchanger (length, diameter, and effectiveness) and gas type (nitrogen, oxygen, and argon). Theoretical results for nitrogen, oxygen, and argon at initial pressure of 25 MPa, initial temperature of 20ºC, indicate that the final temperature equal to (-16.46ºC, −37.34ºC and −56.75ºC) respectively at single stage JTCS. It also shows the possibility of decreasing the final temperature to (-194ºC, −180.9ºC and −183.8ºC) respectively at multistage JTCS. The experimental rig has been constructed for satisfying mathematical model. The experimental results for nitrogen gas show a temperature drop of 6.5ºC when the initial pressure and temperature were 3 MPa and 20ºC respectively. Theoretical results were validated using experimental measurements on the other hand. The computer program has been built to carry out the analysis required for solving the parameters of JTCS under different operations conditions with good agreement compared to recent published researchers.

UR - http://www.scopus.com/inward/record.url?partnerID=8YFLogxK&scp=85191407519

U2 - 10.1016/j.egyr.2024.04.034

DO - 10.1016/j.egyr.2024.04.034

M3 - Article

VL - 11

SP - 4572

EP - 4586

JO - Energy Reports

JF - Energy Reports

SN - 2352-4847

ER -

ID: 56651023