Numerical study of using dean vortices to enhance the film cooling performance for fan shaped hole

被引:13
作者
Chen, Pingting [1 ]
Shi, Wei [1 ]
Li, Xueying [1 ]
Ren, Jing [1 ]
Jiang, Hongde [1 ]
机构
[1] Tsinghua Univ, Dept Energy & Power Engn, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
Dean vortices; Shaped hole; Heat transfer; Additive manufacture; Film cooling; CURVED CHANNEL; HEAT-TRANSFER;
D O I
10.1016/j.ijthermalsci.2021.106913
中图分类号
O414.1 [热力学];
学科分类号
摘要
With the maturing of additive manufacture anticipated in the future, more freedom in film cooling hole design will be obtained. Exploiting this freedom, the present authors designed a new film cooling hole using curved holes to generate Dean Vortices within the fan-shaped hole?s delivery line. The Dean Vortices interacts with the kidney vortices in the coolant and mainstream mixing region. Numerical results, including the film cooling effectiveness values (q), the flow field, heat transfer coefficients (h), and the net heat flux reduction (NHFR) are compared between a laidback, fan-shaped hole (SH), the curved shaped hole (CSH), the reversed curved shaped hole (RCSH) and the round hole (RH) with blowing ratio, M, of 0.5, 1.0, 1.5, 2.0 and 2.5. The comparison shows that film cooling effectiveness values with the CSH and RCSH are higher than the SH or the RH at every M studied. Due to the high kinetic energy transferred to the near-wall region for the CSH and RCSH cases, there is h enhancement on the surface, however. Nevertheless, the CSH and RCSH still display higher NHFR at every M studied than the SH or the RH cases. ANSYS CFX 18.2 and the RNG k-e model equations were employed to do the simulations.
引用
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页数:26
相关论文
共 41 条
[1]  
ANSYS Inc, 2017, ANSYS CFX SOLV THEOR, V18
[2]   Additive manufacturing methods and modelling approaches: a critical review [J].
Bikas, H. ;
Stavropoulos, P. ;
Chryssolouris, G. .
INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2016, 83 (1-4) :389-405
[3]   A review of shaped hole turbine film-cooling technology [J].
Bunker, RS .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2005, 127 (04) :441-453
[4]  
Chen P., 2019, J TURBOMACH, V142, P1
[5]   Cooling effectiveness and aerodynamic performance in a 2D-Contoured endwall passage with different mass flow ratios [J].
Chen, Pingting ;
Alqefl, Mahmood ;
Li, Xueying ;
Ren, Jing ;
Jiang, Hongde ;
Simon, Terrence .
INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2019, 142 :233-246
[6]   Geometrical Optimization and Experimental Validation of a Tripod Film Cooling Hole With Asymmetric Side Holes [J].
Chi, Zhongran ;
Ren, Jing ;
Jiang, Hongde ;
Zang, Shusheng .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2016, 138 (06)
[7]  
Conner B.P., 2014, ADDIT MANUF, V1, P64, DOI DOI 10.1016/J.ADDMA.2014.08.005
[8]   Film Cooling From a Row of Holes Supplemented With Antivortex Holes [J].
Dhungel, Alok ;
Lu, Yiping ;
Phillips, Wynn ;
Ekkad, Srinath V. ;
Heidmann, James .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 131 (02)
[9]  
Fraas M., 2017, TURBO EXPO POWER LAN
[10]   Metal Additive Manufacturing: A Review [J].
Frazier, William E. .
JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, 2014, 23 (06) :1917-1928