TY - JOUR
T1 - Research on enhancing impingement structure heat transfer capability based on secondary impingement
AU - Li, Xinlei
AU - Zhu, Huiren
AU - Liu, Cunliang
AU - Ye, Lin
AU - Xu, Zhipeng
AU - Li, Guodong
AU - Xu, Weijiang
N1 - Publisher Copyright:
© 2025
PY - 2025/5
Y1 - 2025/5
N2 - Impingement structure, renowned for its compact design and exceptional heat transfer capabilities, finds widespread application in diverse cooling systems. The presence of ribs and the prevailing crossflow conditions exert a significant influence on the flow and heat transfer characteristics of the impingement. This study employs the k−wSST turbulence model to numerically investigate the performance of a single-nozzle impingement with a ribbed target. Experimental validation, conducted using the steady-state copper block method, ensures the accuracy of the numerical simulations. By delving into the secondary impact phenomenon induced by the ribs, a step rib configuration is proposed to enhance heat transfer. The optimal rib arrangement under varying crossflow conditions is also explored. The findings reveal that step ribs can effectively elevate the Nuwave and the Nupave by 7.67 % and 25.47 %, compared to a smooth target. This improvement underscores that the enhancement in heat transfer performance is not solely attributed to an increased heat transfer area but also benefits from favorable aerodynamic effects. The optimal rib placement varies with different crossflow conditions. Under low crossflow conditions, the most advantageous rib positioning coincides with the region influenced by the crossflow stagnation point. Conversely, at high crossflow conditions, the optimal rib placement is upstream of the impingement jet.
AB - Impingement structure, renowned for its compact design and exceptional heat transfer capabilities, finds widespread application in diverse cooling systems. The presence of ribs and the prevailing crossflow conditions exert a significant influence on the flow and heat transfer characteristics of the impingement. This study employs the k−wSST turbulence model to numerically investigate the performance of a single-nozzle impingement with a ribbed target. Experimental validation, conducted using the steady-state copper block method, ensures the accuracy of the numerical simulations. By delving into the secondary impact phenomenon induced by the ribs, a step rib configuration is proposed to enhance heat transfer. The optimal rib arrangement under varying crossflow conditions is also explored. The findings reveal that step ribs can effectively elevate the Nuwave and the Nupave by 7.67 % and 25.47 %, compared to a smooth target. This improvement underscores that the enhancement in heat transfer performance is not solely attributed to an increased heat transfer area but also benefits from favorable aerodynamic effects. The optimal rib placement varies with different crossflow conditions. Under low crossflow conditions, the most advantageous rib positioning coincides with the region influenced by the crossflow stagnation point. Conversely, at high crossflow conditions, the optimal rib placement is upstream of the impingement jet.
KW - Jet impingement cooling
KW - Jet-to-crossflow interactions
KW - Overall thermal performance
KW - Ribbed target plate
UR - http://www.scopus.com/inward/record.url?scp=85214329886&partnerID=8YFLogxK
U2 - 10.1016/j.ijthermalsci.2025.109695
DO - 10.1016/j.ijthermalsci.2025.109695
M3 - 文章
AN - SCOPUS:85214329886
SN - 1290-0729
VL - 211
JO - International Journal of Thermal Sciences
JF - International Journal of Thermal Sciences
M1 - 109695
ER -