MAO Shang, LIU Deshu, GUO Qing, WU Xuehong, WANG Yanling, LIU Yong, ZHOU Tao. Numerical Study on Flow and Heat Transfer of Supercritical CO2 in Narrow Rectangular Channel with Sinusoidal RibJ. Atomic Energy Science and Technology. DOI: 10.7538/yzk.2025.youxian.0734
Citation: MAO Shang, LIU Deshu, GUO Qing, WU Xuehong, WANG Yanling, LIU Yong, ZHOU Tao. Numerical Study on Flow and Heat Transfer of Supercritical CO2 in Narrow Rectangular Channel with Sinusoidal RibJ. Atomic Energy Science and Technology. DOI: 10.7538/yzk.2025.youxian.0734

Numerical Study on Flow and Heat Transfer of Supercritical CO2 in Narrow Rectangular Channel with Sinusoidal Rib

  • The efficient heat transfer of supercritical CO2 (SCO2) is crucial for the design and operation of compact heat exchangers in advanced energy systems, such as solar thermal power plants and nuclear reactors. Sinusoidal rib structures are promising for enhancing heat transfer in narrow rectangular channels, yet their comprehensive influence on the flow and heat transfer characteristics of SCO2 remains insufficiently explored. This study aims to investigate the effect of sinusoidal ribs and operating conditions on flow dynamics and heat transfer performance of SCO2 in narrow rectangular channels. A numerical simulation was conducted to analyze the flow and heat transfer processes of SCO2 in a narrow rectangular channel equipped with sinusoidal ribs. The SST k-ω turbulence model was adopted to accurately capture the turbulent flow features and near-wall heat transfer behaviors, considering the strong thermophysical property variations of SCO2 near the critical point. The parameters of the sinusoidal rib structure were analyzed, including amplitude A ranging from 2 mm to 4 mm, period p ranging from 20 mm to 60 mm and operating parameters, including mass flux G ranging from300 kg/(m2·s) to 500 kg/(m2·s), inlet temperature Tin ranging from 300 K to 320 K, heat flux q ranging from 20 kW/m2 to 40 kW/m2 and operating pressure P ranging from 8 MPa to10 MPa. Detailed flow field and temperature distribution data were obtained through numerical simulations to evaluate key performance indicators, such as average heat transfer coefficient (have), average wall temperature (Tw,ave), maximum wall temperature (Tw,max), and performance evaluation criterion (PEC). Results indicate that the have increases with rising G due to stronger turbulent convection. In relation to Tin, have shows a non-monotonic trend, initially increasing as Tin approaches the pseudo-critical temperature (Tpc) and then decreasing. Both increased q and P generally lead to a reduction in have, attributed to the alteration of thermophysical properties. The sinusoidal rib structures enhance heat transfer performance primarily by intensifying near-wall turbulence and disrupting the thermal boundary layer, which promotes the convective heat transfer between SCO2 and the channel wall. Comparative analysis of different rib configurations reveals that the configuration with A=4 mm and p=40 mm achieves the optimal enhanced heat transfer performance in terms of Tw,ave and have. However, when considering Tw,max and PEC, the configuration A=2 mm and p=20 mm outperforms others, yielding the lowest Tw,max=342.29 K and the optimal PEC=1.20. These findings provide a crucial theoretical basis and practical design references for the application of sinusoidal rib structures in high-efficiency compact SCO2 heat exchangers, facilitating the optimization of energy conversion efficiency in advanced energy systems.
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