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Effect of Rotation on Heat Transfer in Rectangular Channels with Pin Fins

机译:旋转对带翅片矩形通道中传热的影响

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The effect of rotation on smooth narrow rectangular channels and narrow rectangular channels with pin fins is investigated in this study. Pin fins are commonly used in the narrow sections within the trailing edge of the turbine blade; the pin fins act as turbulators to enhance internal cooling while providing structural support in this narrow section of the blade. The rectangular channel is oriented at 150 deg with respect to the plane of rotation, and flow through the channel is radially outward. The focus of the study involves narrow channels with aspect ratios of 4:1 and 8:1. The enhancement due to both conducting (copper) pin fins and nonconducting (Plexiglas~(~R)) pins is investigated. Because of the varying aspect ratio of the channel, the height-to-diameter ratio (h_p/D_p) of the pins varies from two, for an aspect ratio of 4:1, to unity, for an aspect ratio of 8:1. A staggered array of pins with uniform streamwise and spanwise spacing (x_p/D_p = s_p/D_p = 2.0) is studied. With this array, 42 pin fins are used, giving a projected surface density of 3.5 pins/in.~2 (0.543 pins/cm~2), for the leading or trailing surfaces. The range of flow parameters include Reynolds number (Re_(Dh) = 5 X 10~3-2 x 10~4), rotation number (Ro = 0.0-0.302), and inlet coolant-to-wall density ratio (Δρ/ρ = 0.12). Heat transfer in a stationary pin fin channel can be enhanced up to 3.8 times that of a smooth channel. Rotation enhances the heat transferred from the pin fin channels to 1.5 times that of the stationary pin fin channels. Overall, rotation enhances the heat transfer from all surfaces in both the smooth and pin fin channels. Finally, as the rotation number increases, spanwise variation increases in all channels.
机译:在这项研究中,研究了旋转对光滑窄矩形通道和带销鳍的窄矩形通道的影响。销翅片通常用于涡轮机叶片后缘内的狭窄区域。针状鳍片充当湍流器,以增强内部冷却,同时在叶片的狭窄部分提供结构支撑。矩形通道相对于旋转平面定向为150度,并且流经该通道的流体径向向外。该研究的重点涉及纵横比为4:1和8:1的狭窄通道。研究了由于导电(铜)引脚鳍和非导电(Plexiglas〜(〜R))引脚引起的增强。由于通道的长宽比变化,对于4:1的长径比,销的高径比(h_p / D_p)从2变为8:1的一体。研究了沿流向和跨向间距均匀的交错排列的引脚阵列(x_p / D_p = s_p / D_p = 2.0)。在此阵列中,使用了42针鳍,对于前表面或后表面,投影表面密度为3.5针/英寸〜2(0.543针/厘米〜2)。流量参数范围包括雷诺数(Re_(Dh)= 5 X 10〜3-2 x 10〜4),转数(Ro = 0.0-0.302)和入口冷却剂与壁的密度比(Δρ/ρ) = 0.12)。固定销翅片通道中的热传递可以提高到平滑通道中的3.8倍。旋转将热量从针状翅片通道转移到静止的针状翅片通道的1.5倍。总体而言,旋转增强了从光滑表面和针翅通道中所有表面的传热。最终,随着转数的增加,所有通道的翼展方向变化都会增加。

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