Author
Listed:
- Weiwei Cui
(College of Energy Storage Technology, Shandong University of Science and Technology, Qingdao 266590, China)
- Zongming Li
(College of Civil Engineering and Architecture, Shandong University of Science and Technology, Qingdao 266590, China)
- Xiaorong Xiang
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China)
- Guoli Pang
(College of Civil Engineering and Architecture, Shandong University of Science and Technology, Qingdao 266590, China)
- Laishun Yang
(College of Energy Storage Technology, Shandong University of Science and Technology, Qingdao 266590, China)
Abstract
A physical model for the precooler in a SABRE engine was established, and both the influencing degrees and physical mechanisms of inlet conditions and geometric parameters on the flow-heat transfer characteristics of the precooler unit were explored through parametric analysis and sensitivity analysis, respectively. The results demonstrated that the air massflow rate exerted the greatest influence on the total pressure loss coefficient of the precooler unit due to its significant impact on airflow velocity and thermal loading. The inlet total temperature had a dominant effect on heat transfer rate, owing to its substantial influence on air viscosity and thermal loading. Furthermore, both alone and in combination with air massflow rate, inlet total pressure exhibited a greater impact on total pressure loss of precooler unit compared to inlet total temperature and its coupling effects with air massflow rate. In contrast, both air massflow rate and its coupling effects with inlet total temperature significantly affected the heat transfer rate. On the other hand, tube spacing had the most significant impact on both the total pressure loss coefficient and heat transfer rate due to its substantial influence on air throughflow area and acceleration between microtubes. Moreover, the number of tube rows played a predominant role in determining the heat transfer rate of the precooler unit as it caused significant changes in the contact area between the hot air and the microtubes, as well as airflow velocity. However, only two geometric interaction terms (corresponding to interactions between the number of tube rows and tube spacing, as well as between tube spacing and tube diameter) significantly affected the total pressure loss coefficient, and no interaction term was found to be significant for influencing the heat transfer rate. Eventually, two optimal schemes involving inlet conditions and geometric parameters were established to enhance the flow-heat transfer characteristics of the precooler unit.
Suggested Citation
Weiwei Cui & Zongming Li & Xiaorong Xiang & Guoli Pang & Laishun Yang, 2024.
"Sensitivities of Geometric Parameters and Inlet Conditions on the Flow-Heat Characteristics of the Precooler in SABRE,"
Energies, MDPI, vol. 17(23), pages 1-23, November.
Handle:
RePEc:gam:jeners:v:17:y:2024:i:23:p:5890-:d:1527943
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