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Accident? The reasons could have been multi-fold. But, under this scenario, the main culprit could have been the spreading resistance that was overlooked during the design process. It is very important for heat sink users to realize that, unless the heat sink is custom developed for a specific application, thermal performance values provided in vendor's catalogs rarely account for the additional resistances coming from the size and location considerations of a heat source. It is understandable that the vendors themselves could not possibly know what kind of devices the users will be cooling with their products. Introduction In cases where the footprint of a heat sink need not be much larger than the size of the heat source, the contribution of the spreading resistance to the overall device temperature rise may be insignificant and usually falls within the design margin. However, in an attempt to remove more heat from today's high performance devices, a larger heat sink is often used and, consequently, the impact of spreading resistance on the performance of a heat sink is becoming an important factor that must not be ignored in the design process. It is not uncommon to find in many high performance, high power applications that more than half the total temperature rise of a heat sink is attributed to the spreading resistance in the base-plate. The objectives of this article are: 1) to understand the physics and parameters associated with spreading resistance 2) to provide a simple design correlation for accurate prediction of the resistance 3) to discuss and clarify the concept of spreading resistance with an emphasis on the practical use of the correlation in heat sink applications The correlation provided herein was originally developed in references 1 and 2. This article is an extension of the earlier presentation. Spreading Resistance The spreading resistance can be determined from the following set of parameters:
We will assume, for the time being, that the heat source is centrally mounted on the base-plate, and the heat sink is cooled uniformly over the exposed finned surface. These two assumptions will be examined in further detail. Figure 2 shows a two-dimensional side view of the heat sink with heat-flow lines schematically drawn in the base-plate whose thickness is greatly exaggerated. At the top, the corresponding surface temperature variation across the center line of the base-plate is shown by the solid line. The dotted line represents the average temperature of the surface which is, again, independent of the heat source size and can be easily determined by multiplying R0 with the total amount of heat dissipation, denoted as Q. As indicated in Fig. 2, the maximum constriction resistance Rc, which accounts for the local temperature rise over the average surface temperature, is the only additional quantity that is needed for determining the maximum heat sink temperature. It can be accurately determined from the following correlation.
Note that the correlation addresses neither the shape of the heat source nor that of the heat sink base-plate. It was found in the earlier study that this correlation typically results in an accuracy of approximately 5% over a wide range of applications with many combinations of different source/sink shapes, provided that the aspect ratio of the shapes involved does not exceed 2.5. See references 1 and 2 for further discussions. Example Problem Solutions
Therefore, Hence, the maximum resistance, Rtotal , is: Rtotal = Ro + Rc = 1.0 + 0.66 = 1.66 °C/W Readers should note the far right temperature distribution in Fig. 1 which is the result of a numerical simulation for the present problem in rectangular coordinates. Effect of Source Location
Figure 3 - Heat-sink local resistance showing the effect of source location: from L to R, heat source at (37.5,0) and (37.5,37.5) the first one is for the case where the heat source is mounted midway along the edge, and the other, where it is mounted on one corner of the heat sink. For these two special cases, the maximum spreading resistance can be calculated by using Eq. (1) for Rc with input parameters t and R0 modified as shown below:
with For other intermediate source locations, numerical simulations were carried out and a plot is provided in Fig. 4 for the correction factor Cf which can be used to compute the total resistance as
where Rc is determined from Eq. (1), given for the case with the heat source placed at the center. ![]() Figure 4 - Correction factor as a function of source location The coordinates in Fig. 4 indicate the location of the center of the heat source measured from the center of the base-plate in mm: the case with a centrally located heat source corresponds to (0,0), and the cases shown in Fig. 3 correspond to (37.5,0) and (37.5,37.5) for the first and second cases, respectively. Only one quadrant is shown in Fig. 4 as they would be, owing to the assumption of uniform cooling, symmetrical about (0,0). As can be seen from the figure, the correction factor increases from 1 as the heat source is placed away from the center. It is worthwhile noting that the increase is, however, very minimal over a wide region near the center, and most increases occur closer to the edges. Unlike C in the earlier expression, Cf is case dependent (i.e. it depends on the heat-source size). However, it was found that the plots of Cf obtained for many other cases exhibit essentially the same profile as that shown in Fig. 4, with magnitudes at the corners determined from Eq. (3), and the domain of the plot defined by the maximum displacement of the heat source. Based on this observation, a general conclusion can be made: for all practical purposes, as long as the heat source is placed closer to the center than to the edges of the heat sink, the correctional increase in the spreading resistance may be ignored, and Cf =1 may be used. As noted above, this would introduce a small error of no greater than 5-10% in the spreading resistance which, in turn, is a fraction of the total resistance. So far, we have assumed a uniform cooling over the entire finned-surface area of the base-plate. Although this is a useful assumption, it is seldom realized in actual situations. It is well known that, due to the thinner boundary layer and the less down-stream heating effect, a device would be cooled more effectively if it is mounted toward the air inlet side. Again, a numerical simulation is carried out using our example problem with the boundary layer effect included. Figure 5 shows the resulting modified correction factor as a function of the distance from the center of the heat sink to the heat source placed along the center line at y=0: x = -37.5 mm corresponds to the front most leading edge location of the heat source and x = 37.5 mm the rear most trailing edge placement. ![]() Figure 5 - Correction factor modified for boundary layer effect at y=0 As can be seen from the figure, it is possible to realize a small improvement by placing the heat source forward of the center location where Cf < 1. However, it was experienced in practice that accommodating a heat source away from the center and ensuring its mounting orientation often cause additional problems during manufacturing and assembly processes. Summary and Discussion The earlier study revealed that, depending on the relative magnitude of the average heat sink resistance, the spreading resistance may either increase or decrease with the base-plate thickness. If the heat sink resistance is sufficiently small, as in liquid cooled heat sink applications, the spreading resistance always increases with the thickness, and an optimum thickness does not exist. On the other hand, if the heat sink resistance is large, as experienced in most air-cooled applications, the spreading resistance decreases with the thickness and a finite optimum thickness exists. It is to be noted that the present correlation calculates the spreading resistance only in the base-plate and does not account for the effect of additional spreading that may exist in other places, such as the fins in a planar heat sink. This additional spreading in the fins usually affects the spreading resistance in a similar way to a thicker base-plate. The current author found that an increase of 20% in the base-plate thickness during the calculation roughly accounts for the effect of this additional spreading in the fins of the same material for most planar heat sinks under air cooling. No modification is required for pin-fin heat sinks. Seri Lee References
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