TY - JOUR
T1 - Thermal analysis of supercritical CO2 in a horizontal circular tube subjected to axially non-uniform heating
AU - Li, Chao
AU - Xie, Gongnan
AU - Yang, Jinhong
AU - Boetcher, Sandra K.S.
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2025/8/15
Y1 - 2025/8/15
N2 - During flight, aircraft engine pre-cooler pipes typically experience uniform heating under stable external conditions. However, sudden environmental changes can introduce axially non-uniform heat flux, a scenario that remains underexplored in existing research. This numerical study investigates the flow and heat transfer characteristics of supercritical carbon dioxide (sCO2) in a horizontal circular tube subjected to non-uniform axial heat flux conditions: monotonically decreasing (Type (a)) and monotonically increasing (Type (b)). Using the standard k-ε turbulence model with enhanced wall treatment, the study achieves reasonable wall temperature predictions compared to experimental data. Results highlight complex heat transfer behaviors under non-uniform heating compared to the uniform heat flux case (Type (c)). In Type (a) cases, heat transfer deterioration (HTD) near the inlet intensifies with increasing heat flux amplitude (Ai), with secondary flow effects playing a crucial role. Specifically, a vortex near the top wall impedes heat transfer, exacerbating HTD when Tb = Tpc. As Ai increases, the vortex center shifts closer to the top wall, intensifying the phenomenon. In contrast, HTD is absent in Types (b) and (c) at Tb = Tpc. Additionally, regions with high secondary flow kinetic energy (K > 5) are localized along y-axis symmetric walls, with peak K values increasing as heat flux rises at Tb = Tpc. These findings provide new insights into non-uniform heating effects in sCO2 cooling systems, which are critical for aircraft thermal management.
AB - During flight, aircraft engine pre-cooler pipes typically experience uniform heating under stable external conditions. However, sudden environmental changes can introduce axially non-uniform heat flux, a scenario that remains underexplored in existing research. This numerical study investigates the flow and heat transfer characteristics of supercritical carbon dioxide (sCO2) in a horizontal circular tube subjected to non-uniform axial heat flux conditions: monotonically decreasing (Type (a)) and monotonically increasing (Type (b)). Using the standard k-ε turbulence model with enhanced wall treatment, the study achieves reasonable wall temperature predictions compared to experimental data. Results highlight complex heat transfer behaviors under non-uniform heating compared to the uniform heat flux case (Type (c)). In Type (a) cases, heat transfer deterioration (HTD) near the inlet intensifies with increasing heat flux amplitude (Ai), with secondary flow effects playing a crucial role. Specifically, a vortex near the top wall impedes heat transfer, exacerbating HTD when Tb = Tpc. As Ai increases, the vortex center shifts closer to the top wall, intensifying the phenomenon. In contrast, HTD is absent in Types (b) and (c) at Tb = Tpc. Additionally, regions with high secondary flow kinetic energy (K > 5) are localized along y-axis symmetric walls, with peak K values increasing as heat flux rises at Tb = Tpc. These findings provide new insights into non-uniform heating effects in sCO2 cooling systems, which are critical for aircraft thermal management.
KW - Heat transfer deterioration
KW - Non-uniform heat flux
KW - Secondary flow
KW - Supercritical carbon dioxide
KW - Temperature gradient
UR - http://www.scopus.com/inward/record.url?scp=105002655617&partnerID=8YFLogxK
U2 - 10.1016/j.applthermaleng.2025.126285
DO - 10.1016/j.applthermaleng.2025.126285
M3 - 文章
AN - SCOPUS:105002655617
SN - 1359-4311
VL - 273
JO - Applied Thermal Engineering
JF - Applied Thermal Engineering
M1 - 126285
ER -