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A novel approach to heat transfer enhancement using trapezoid shaped spiral strips to promote tumble and swirl in a slot shaped channel used in heat exchangers

机译:一种使用梯形形状螺旋条传热增强的新方法,以促进热交换器中使用的槽形通道中的滚动和旋转

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Heat transfer results for a given slot shaped channel with a 3:1 aspect ratio are presented using various configurations of a trapezoid shaped spiral wound strips to enhance swirl and tumble motion in the channel. The Reynolds numbers investigated range from 10,000 to 50,000 and are based on the characteristics of the fluid at the channel inlet. The ratio of absolute temperatures between the wall and fluid are on the order of 0.8 to 0.9. A combination of thermochromic liquid crystal techniques and thermocouples were used to create a temperature vs. time map. Duhamel's superposition theorem was then used to determine the local heat transfer coefficients (h) and heat transfer enhancement factors (Nu/Nu_o). In one series of testing a straight center inlet with a radiused entry was used to reduce entry effects. In a second series of test a 90 degree inlet geometry was used to enhance turbulence at the entry. Three combinations of helical strips were tested using a single, double, and pentuple spiral design. The pitch of the helix remained constant in all tests at 0.75" (18 mm) as well as the height of the strip at 0.0625" (1.6 mm), yielding a p/e (pitch/rib height) ratio of 12. The resulting flow in the channel creates a tumble motion as the main channel fluid encounters the strips and a swirl motion as the fluid is directed through the spiraling helix. Many studies involving heat transfer using swirl enhancement have been presented in literature using round passages with wire spring inserts or twisted tapes, typically used in heat exchangers. In turbine aero foils, particularly in the mid-span region, rectangular channels with various configurations of trip strips are used to enhance heat transfer. The results of the tests presented in this paper show local heat transfer enhancement (Nu/NU_o) values greater than seven and subsequent average values for the entire channel greater than three at the higher Reynolds numbers along with relatively low normalized friction factors.
机译:使用梯形形状螺旋缠绕条的各种构造来提出具有3:1纵横比的给定槽形沟道的传热结果,以增强通道中的旋转和翻滚运动。 Reynolds数字调查了10,000至50,000的范围,并且基于通道入口处的流体的特性。壁和流体之间的绝对温度与0.8至0.9的比率约为0.9。热致变色液晶技术和热电偶的组合用于产生温度与时间映射。然后使用Duhamel的叠加定理来确定局部传热系数(H)和传热增强因子(NU / NU_O)。在一系列测试中,使用辐射入口的直中心入口用于减少进入效果。在第二系列测试中,使用90度入口几何形状来增强进入的湍流。使用单一,双和闪烁的螺旋设计测试了三种螺旋条组合。螺旋的间距在0.75“(18 mm)的所有测试中保持恒定,以及条带的高度为0.0625”(1.6毫米),产生AP / E(俯仰/肋高度)比为12.所得流动在通道中,当主沟道流体遇到条带和旋涡运动时,在螺旋螺旋中引导时,在沟道中产生翻滚运动。涉及使用旋流增强的热传递的许多研究已经在文献中呈现使用圆形通道,其中圆形通道或通常用于热交换器中的绞合带。在涡轮机Aero箔中,特别是在中跨区域中,使用具有各种跳闸条配置的矩形通道来增强传热。本文中提出的测试结果显示了局部传热增强(NU / NU_O)值大于七个和随后的整个通道的平均值,在较高的雷诺数的整个通道上大于三个,以及相对低的标准化摩擦因子。

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