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Experimental investigation of the thermal-hydraulic characteristics of liquid cooling heat sinks with novel pin fins
被引:4
作者:
Wang, Jiale
[1
]
Qi, Shaohuan
[1
]
Xu, Zhaohao
[1
]
Xu, Yu
[1
]
机构:
[1] Nanjing Univ Aeronaut & Astronaut, Key Lab Aircraft Environm Control & Life Support, MIIT, 29 Yudao St, Nanjing 210016, Peoples R China
基金:
中国国家自然科学基金;
中国博士后科学基金;
关键词:
Pin fin;
Heat sink;
Petaloid;
Pinwheel-like;
Honeycombed;
Thermal-hydraulic characteristics;
FLOW;
PERFORMANCE;
NANOFLUID;
SHAPE;
D O I:
10.1016/j.csite.2024.104172
中图分类号:
O414.1 [热力学];
学科分类号:
摘要:
Pin-fin heat sinks (PFHSs) in single-phase liquid cooling systems possess significant potential for extracting higher levels of heat from avionics. However, there is a scarcity of investigations on PFHSs with innovative pin fin shapes. Here, petaloid I and II, pinwheel-like, and honeycombed shapes were designed, and their thermal-hydraulic characteristics were examined under inlet temperatures of 10 and 20 degrees C, flow rates of 400-2000 mL/min, and heat fluxes of 60-150 kW/m2. Among these PFHSs, the honeycombed shape exhibited the highest heat transfer coefficient, followed by the pinwheel-like shape; they also displayed the lowest wall temperature. However, their Nusselt numbers were lower than those of petaloid heat sink I. The Nusselt number of each heat sink exhibited a downward trend with the increasing inlet temperature and heat flux, while the friction factor remained largely unaffected. The performances were evaluated by a comprehensive factor, and the honeycombed PFHS ranked first. New correlations for the Nusselt number and friction factor of these PFHSs were developed. The mean absolute deviations were all less than 5%, with most predicted values falling within the +/- 5% range compared to experimental values. These novel heat sinks are crucial for enhancing the performance of airborne liquid cooling systems.
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页数:15
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