首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >STUDY ON CONJUGATE THERMAL PERFORMANCE OF A STEAM-COOLED RIBBED CHANNEL WITH THICK METALLIC WALLS
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STUDY ON CONJUGATE THERMAL PERFORMANCE OF A STEAM-COOLED RIBBED CHANNEL WITH THICK METALLIC WALLS

机译:厚金属壁蒸汽冷却肋通道的共轭热性能研究

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In this work, a conjugate heat transfer model was established to numerically investigate the conjugate thermal performance of a steam-cooled ribbed channel with thick metallic walls. By employing the software of ANSI'S CFX, the flow field in the channel and the temperature field in the solid channel were calculated. The flow behavior, heat transfer performance and temperature gradient distributions of ribbed channels with wall thickness (δ) of 1 - 5 mm, rib height-to-hydraulic diameter (e/D) of 0.047 - 0.188, rib pitch-to-height ratio (P/e) of 5 -15 and rib angle-of-attack (a) of 30° - 90° were compared and analyzed. The optimum structure parameters of thick-wall ribbed channel with higher heat transfer performance and lower maximum temperature gradient were obtained. The results show that the SST k-co turbulence model is more suitable for the conjugate heat transfer problem of steam in the thick-wall ribbed channels. The friction factor reduces gradually with the increase of Re, increases greatly with the increase of e/D and a, and first increases then decreases with the increase of P/e. The average Nusselt number increases up to 8.81 times, while the maximum temperature gradient decreases about 45.35% when Reynolds number varies from 10,000 to 70,000. The rib angle of about 45°-60°, e/D of 0.188, and P/e of 10 are suitable to obtain the optimum thermal performance of steam flow in the ribbed channel. The influence of 3 on the flow and heat transfer characteristics is non-significant.
机译:在这项工作中,建立了共轭传热模型以用厚金属壁进行数值研究蒸汽冷罗纹通道的共轭热性能。通过采用ANSI的CFX软件,计算通道中的流场和实际通道中的温度场。具有1-5mm的壁厚(δ),肋骨高度到液压直径(E / D)为0.047- 0.188,肋间距到高度比的流动性能,传热性能和温度梯度分布(P / E)为5 -15和肋骨 - 攻击(A)的30° - 90°,并分析。获得了具有较高传热性能和较低最大温度梯度的厚壁肋沟道的最佳结构参数。结果表明,SST k-Co湍流模型更适合于厚壁罗纹通道中蒸汽的缀合物传热问题。随着RE的增加,摩擦因子逐渐减少,随着E / D的增加,大大增加,然后随着P / E的增加而降低。当雷诺数从10,000到70,000变化时,平均露天数量增加高达8.81倍,而最高温度梯度降低约45.35%。肋角约为45°-60°,E / D为0.188,P / E的10个适用于肋状通道中的蒸汽流动的最佳热性能。 3对流动和传热特性的影响是非显着的。

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