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Research Papers

Viscous Scaling Phenomena in Miniature Centrifugal Flow Cooling Fans: Theory, Experiments and Correlation

[+] Author and Article Information
Patrick A. Walsh, Edmond J. Walsh, Ronan Grimes

Department of Mechanical and Aeronautical Engineering, Stokes Institute, University of Limerick, Limerick, Ireland

J. Electron. Packag 132(2), 021001 (May 19, 2010) (8 pages) doi:10.1115/1.4001590 History: Received June 09, 2009; Revised January 26, 2010; Published May 19, 2010; Online May 19, 2010

This paper analyzes the scale effects that occur in miniature centrifugal flow fans and investigates the possibility of optimizing blade geometry so that performance can be enhanced. Such fans are typically employed in small scale heat sinks such as those used for processor cooling applications or in portable electronics. The specific design parameter varied is the blade chord length, and the resulting fan performance is gauged by examining the flow rate, pressure rise, and power consumption characteristics. The former two are measured using a BS 848 fan characterization rig and the latter, by directly measuring the power consumed. These characteristics are studied for three sets of scaled fans with diameters of 15 mm, 24 mm, and 30 mm, and each set considers six individual blade chord lengths. A novel theory is put forward to explain the anticipated effect of changing this parameter, and the results are analyzed in terms of the relevant dimensionless parameters: Reynolds number, chord length to diameter of fan ratio, flow coefficient, pressure coefficient, and power coefficient. When these characteristic parameters are plotted against the Reynolds number, similar trends are observed as the chord length is varied in all sets of scaled fans. The results show that the flow coefficient for all the miniature fans degrade at low Re values, but the onset of this degradation was observed at higher Re values for longer blade chord designs. Conversely, it was found that the pressure coefficient is elevated at low Re, and the onset Re for this phenomenon correlates well with the drop off in flow coefficient. Finally, the trend in power coefficient data is similar to that for the flow coefficient. The derived theory is used to correlate this data for which all data points fall within 6% of the correlation. Overall, the findings reported herein provide a good understanding of how changing the blade chord length affects the performance of miniature centrifugal fans; hence, providing fan designers with guidelines to aid in developing optimum blade designs, which minimize adverse scaling phenomena.

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Copyright © 2010 by American Society of Mechanical Engineers
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Figures

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Figure 3

Plot of Eq. 11 depicting the effect of changing the value of a on the flow rate and flow coefficient when the BL thickness become comparable with the width of the blade passage, i.e., as NBL approaches unity

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Figure 4

Photograph showing all fans used during experimentation, blade chord length increasing from left-to-right and fan diameter increasing from bottom-to-top

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Figure 5

Schematic of the experimental test facility used to obtain all the flow rate and pressure rise characteristics

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Figure 6

Schematic showing how the fans were positioned on the flow characterization rig during experimentation

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Figure 7

Pressure coefficient versus flow coefficient curves for each of the different fan designs tested, only data from 24 mm fans shown. Available in color online.

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Figure 8

Variation in maximum flow coefficient with chord Reynolds number. Available in color online.

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Figure 9

Data of Fig. 8 in terms of Eq. 10 results in collapsing the data. Available in color online.

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Figure 10

Variation in maximum pressure coefficient with chord Reynolds number. Available in color online.

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Figure 1

Plot depicting boundary layer development on blade surfaces by Blasius’ theory for similar diameter fans with varying chord length and operating at the same rotational speed

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Figure 2

Schematic of radial flow velocity profile between blade passages highlighting the method used to determine the overall mean velocity

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Figure 11

Data of Fig. 1 replotted to illustrate how data is collapsed when plotted in terms of ΦMax(CL/ϕF)−1/4 versus Re0.5(ϕF/CL). Available in color online.

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Figure 12

Variation in maximum power coefficient with ReC for one set of six different chord length fans. Available in color online.

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