Conjugate Heat Transfer Study of Innovative Pin-Fin Cooling Configuration

被引:0
作者
Hossain, Mohammad A. [1 ]
Asar, Munevver E. [1 ]
Ameri, Ali [1 ]
Bons, Jeffrey P. [1 ]
机构
[1] Ohio State Univ, Dept Mech & Aerosp Engn, Columbus, OH 43235 USA
来源
AIAA SCITECH 2020 FORUM | 2020年
关键词
PRESSURE-DROP; ARRAY; IMPINGEMENT; FLOW;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The study involves experimental and numerical heat transfer analyses of four pin-fin cooling configurations in a rectangular channel. Two design concepts were studied with two separate pin-fin (cylindrical and triangular) geometries. The first design includes a single-walled pin-fin (D = 1.5mm) configuration (PF and TF) where the coolant flows through an array of full length (H/D = 1.33) cylindrical and triangular pin-fins. The second configuration involves a double-walled pin-fin-jet configuration (PFC jet and TFC jet) where the coolant jet impinges on the target wall, then flows through the array of partial length (G/D = 0:4) pin-fins. Infrared (IR) thermography was used to measure the wall temperature of the target surface to estimate the overall cooling effectiveness (phi). A transient heat transfer experiment was conducted to evaluate the internal heat transfer coefficient from the transient wall temperature. It is found that the double-walled pin-fin-jet configuration shows higher cooling effectiveness compared to the single-walled pin-fin design. The triangular pin-fin (TF) showed a higher heat transfer augmentation compared to the cylindrical pin-fin (PF) design. Numerical study later confirmed that the triangular pin-fin creates a pair of streamwise vortices that augments the local heat transfer. The presence of the pin-fin in the double-walled configuration prevents the development of a strong crossflow that negatively affects the heat transfer of the impinging jet. In addition, the triangular pin-fin not only prevent the strong crossflow, but redirects the coolant in the lateral direction that eventually contributes to the formation of a counter rotating vortex pair (CRVP) in the streamwise direction thus augments local heat transfer and improves overall cooling effectiveness. Pressure drop measurement showed that the full length triangular pin-fin has a higher pressure loss but the partial length pin-fin can lower the pressure loss considerably without compromising additional cooling performance.
引用
收藏
页数:15
相关论文
共 28 条
[1]   A REVIEW OF STAGGERED ARRAY PIN FIN HEAT-TRANSFER FOR TURBINE COOLING APPLICATIONS [J].
ARMSTRONG, J ;
WINSTANLEY, D .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1988, 110 (01) :94-103
[2]  
CHANCE JL, 1974, TAPPI, V57, P108
[3]   Recent Advances of Internal Cooling Techniques for Gas Turbine Airfoils [J].
Chyu, Minking K. ;
Siw, Sin Chien .
JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2013, 5 (02)
[4]   Convective heat transfer of cubic fin arrays in a narrow channel [J].
Chyu, MK ;
Hsing, YC ;
Natarajan, V .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1998, 120 (02) :362-367
[5]  
Coleman W., 1989, Heat Transfer and Film -Cooling Measurements on a Stator Vane With Fan -Shaped Cooling Holes
[6]   Experiments and modeling of the hydraulic resistance and heat transfer of in-line square pin fin heat sinks with top by-pass flow [J].
Dogruoz, MB ;
Urdaneta, M ;
Ortega, A .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2005, 48 (23-24) :5058-5071
[7]   Effects of Geometry, Spacing, and Number of Pin Fins in Additively Manufactured Microchannel Pin Fin Arrays [J].
Ferster, Katharine K. ;
Kirsch, Kathryn L. ;
Thole, Karen A. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 140 (01)
[8]   STREAMWISE FLOW AND HEAT-TRANSFER DISTRIBUTIONS FOR JET ARRAY IMPINGEMENT WITH CROSS-FLOW [J].
FLORSCHUETZ, LW ;
TRUMAN, CR ;
METZGER, DE .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1981, 103 (02) :337-342
[9]  
Gnielinski V., 1975, Forschung im Ingenieurwesen, V41, P8, DOI [DOI 10.1007/BF02559682, 10.1007/BF02559682]
[10]  
Hussain A. A., 1991, Heat Transfer