Optimal design of divertor heat sink with different geometric configurations of sectorial extended surfaces

2015 ◽  
Vol 100 ◽  
pp. 581-595 ◽  
Author(s):  
Sandeep Rimza ◽  
Kamalakanta Satpathy ◽  
Samir Khirwadkar ◽  
Karupanna Velusamy
2015 ◽  
Vol 32 (2) ◽  
pp. 219-227
Author(s):  
Boo Seong Park ◽  
Hyun Jin Park ◽  
Bo Hung Kim
Keyword(s):  

2013 ◽  
Vol 2 (2) ◽  
pp. 19-22
Author(s):  
Jae-Hyun Kwon ◽  
Jun-Myung Lee ◽  
Wei Huang ◽  
Keon-Jun Park ◽  
Yong-Kab Kim

Author(s):  
Zhigang Gao ◽  
Tianhu Wang ◽  
Yuxin Yang ◽  
Xiaolong Shang ◽  
Junhua Bai ◽  
...  

Abstract The issue of regenerative cooling is one of the most important key technologies of flight vehicles, which is applied into both the engine and high-power electrical equipment. One pattern of regenerative cooling channels is the microchannel heat sinks, which are thought as a prospective means of improving heat removal capacities on electrical equipment of smaller sizes. In this paper, three numerical models with different geometric configurations, namely straight, zigzag, and sinusoid respectively, are built to probe into the thermal hydraulic performance while heat transfer mechanism of supercritical methane in microchannel heat sinks for the heat removal of high-power electromechanical actuator is also explored. In addition, some crucial influence factors on heat transfer such as inlet Reynolds number, operating pressure and heating power are investigated. The calculation results imply the positive effect of wavy configurations on heat transfer and confirm the important effect of buoyancy force of supercritical methane in channels. The heat sinks with wavy channel show obvious advantages on comprehensive thermal performance including overall thermal performance parameter ? and thermal resistance R compared with that of the straight one. The highest Nu and average heat transfer coefficient am appear in the heat sink with zigzag channels, but the pumping power of the heat sink with sinusoidal channels is lower due to the smaller flow loss.


2008 ◽  
Vol 31 (1) ◽  
pp. 184-195 ◽  
Author(s):  
Chyi-Tsong Chen ◽  
Ching-Kuo Wu ◽  
Chyi Hwang

Author(s):  
M. C. Wu ◽  
C. H. Peng ◽  
C. Y. Lee ◽  
C. J. Fang ◽  
Y. H. Hung

The demand for high execution speed and memory capacity for modern computers results in an increasing circuit density per unit chip and high power dissipation per unit volume. Consequently, traditional air cooling technology such as air-cooled heat sink is reaching the limits for electronic applications. Thermoelectric coolers are regarded as potential solutions for enhancing the performance of air-cooled heat sinks. In the present study, a semi-empirical method for exploring the thermal performance of a heat sink integrated with or without TEC has been successfully established. A concept of design of experiments (DOE) is applied, and a statistical method for sensitivity analysis of the influencing parameters is performed to determine the key factors that are critical to the design. By the statistical sensitivity analysis of ANOVA F-test for the temperature reduction (ΔTC−B) and COP of the TEC, the factor contributions of QP, Rext and I are 31.66%, 33.73%, 34.61% as well as 14.9%, 0%, 85.1%, respectively. By employing the gradient-based numerical optimization technique, a series of constrained optimal designs have been performed. Under the given constraints of COP≧2, the optimal value of ΔTC−B (3.3°C) is obtained with the corresponding Qp (31.99W) and Qte (16W). Comparisons between the results by the present optimal design and those obtained by the semi-empirical results have been made with a satisfactory agreement. The present optimal design shows that a heat sink integrated with TEC can extend the upper limits of thermal management for traditional air-cooled heat sinks.


Author(s):  
A. Berkan Erdog˘mus¸ ◽  
Murat S¸ahin ◽  
Ali Murteza C¸olakog˘lu ◽  
Birol Erentu¨rk

In this study, the cooling performance of a flash pumped laser using Nd:YAG was investigated. The examined system is used to cool down the laser head of a range finder device where heat is produced. Three dimensional CFD model for the examined system was generated and the results were verified by using experimental study. The transient approach and k-epsilon turbulence model were used during the computational analysis. It was realized that the result were in good consistency. At the end of the verification, it is found that the use of extended surfaces on the heat sink does not enhance the heat transfer from the surface in 3 minutes during transient phase because of low thermal diffusivity of titanium material and the undesired high temperature values were seen. Then the cooling system was modified. As a result more reliable cooling system is developed. The enlargement of the liquid flow channels increases the heat transfer and reduces the heat sink temperatures with addition of negligible pressure drop.


Sign in / Sign up

Export Citation Format

Share Document