Effect of internal crossflow on impingement cooling flow and heat transfer characteristics

被引:2
作者
Wang, Pengfei [1 ,2 ,3 ]
Liu, Jun [1 ,2 ,3 ]
Wang, Pei [1 ,2 ,3 ]
Liu, Jiajie [1 ,2 ,3 ]
Wang, Haohan [1 ,4 ]
Yang, Wenshuai [1 ,4 ]
Zhu, Junqiang [1 ,2 ,3 ]
机构
[1] Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
[2] Univ Chinese Acad Sci, Sch Aeronaut & Astronaut, Beijing 100049, Peoples R China
[3] Natl Key Lab Sci & Technol Adv Light duty Gas Turb, Beijing 100190, Peoples R China
[4] Jiangsu Univ, Res Ctr Fluid Machinery Engn & Technol, Zhenjiang 212013, Peoples R China
关键词
Impingement cooling; Internal crossflow; External crossflow; Heat transfer; Overall thermal efficiency; JET-IMPINGEMENT; CIRCULAR JET; IMPINGING JET; SURFACE; GAS; PERFORMANCE; ARRAYS;
D O I
10.1016/j.icheatmasstransfer.2024.108119
中图分类号
O414.1 [热力学];
学科分类号
摘要
The flow and heat transfer characteristics of a single-row impingement jet, fed by internal crossflow, are numerically investigated. The results showed that the internal crossflow propels a rapid coolant outflow on the leeward side of the hole, subsequently elevating the local impingement Reynolds number. Concurrently, the internal crossflow augments the heat transfer rate on the impingement target surface, with surges reaching up to 60 % in the local Nu number and 11 % in the average Nu number at low external crossflow. Counter-intuitively, the heat transfer enhancement due to the increase in local Reynolds number diminishes as the strength of the external crossflow increases. This phenomenon is attributed to the emergence of an in-hole counter-rotating vortex pair, whose interaction with the external crossflow induces elongation of the jet in the pitchwise direction. However, these enhancements in heat transfer rate are counterbalanced come at the expense of a more complex flow structure and higher flow losses. The weight of the internal and external crossflow on impingement cooling performance is also investigated using the overall thermal efficiency which considers both heat transfer and flow resistance and it is found that the external crossflow is the main culprit for the decrease in overall thermal efficiency.
引用
收藏
页数:23
相关论文
共 49 条
[31]   IMPINGEMENT COOLING PERFORMANCE IN GAS-TURBINE AIRFOILS INCLUDING EFFECTS OF LEADING EDGE SHARPNESS [J].
METZGER, DE ;
BALTZER, RT ;
JENKINS, CW .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1972, 94 (03) :219-&
[32]  
Obot N.T., 1979, ASME Paper No. WA/HT- 53
[33]   IMPINGEMENT HEAT-TRANSFER WITHIN ARRAYS OF CIRCULAR JETS .1. EFFECTS OF MINIMUM, INTERMEDIATE, AND COMPLETE CROSS-FLOW FOR SMALL AND LARGE SPACINGS [J].
OBOT, NT ;
TRABOLD, TA .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1987, 109 (04) :872-879
[34]   High-Fidelity Simulations of Multi-Jet Impingement Cooling Flows [J].
Otero-Perez, J. Javier ;
Sandberg, Richard D. ;
Mizukami, Satoshi ;
Tanimoto, Koichi .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 143 (08)
[35]   Numerical investigations of heat transfer and pressure drop characteristics in multiple jet impingement system [J].
Penumadu, Prithvi Sai ;
Rao, Arvind Gangoli .
APPLIED THERMAL ENGINEERING, 2017, 110 :1511-1524
[36]   Noncanonical short hole jets-in-crossflow for turbine film cooling [J].
Plesniak, Michael W. .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2006, 73 (03) :474-482
[37]  
Popiel O., 1986, Proc. 8th Int. Heat Transfer, V3, P1187
[38]   Thermal performance assessment of turbulent channel flows over different shaped ribs [J].
Promonge, Pongjet ;
Thianpong, Chinaruk .
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2008, 35 (10) :1327-1334
[39]  
Spring S., 2013, AIAA ASME JOINT THER
[40]   OBLIQUE IMPINGEMENT OF A CIRCULAR JET IN A CROSS-FLOW [J].
STAPOUNTZIS, H .
APPLIED SCIENTIFIC RESEARCH, 1993, 51 (1-2) :231-235