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Turbulent heat transfer in a trapezoidal channel with transverse and v-shaped ribs on two opposite walls

机译:梯形通道中的湍流热传递,在两个相对的壁上具有横向和V形肋

摘要

This study investigates the turbulent heat transfer and friction in a trapezoidalchannel with opposite walls roughened with transverse and v-shaped ribs. Theroughened channel depicts the internal cooling passage of an aerofoil near the trailingedge. The various configurations investigated for this study are smooth channel, channelwith 90? transverse ribs and channel with v-shaped ribs angled at 45?. The pitch-toheightratio (P/e), rib height-to-hydraulic diameter ratio (e/Dh) and the aspect ratio (W/e)were maintained at 12, 0.1906 and 1, respectively. The configuration was tested forReynolds number ranging from 7,000 to 40,000. The 45? rib was found to produce themaximum heat transfer and minimum pressure loss.
机译:这项研究调查了梯形通道中的湍流传热和摩擦,其相对壁被横向和V形肋粗糙化了。粗糙的通道描绘了后缘附近的机翼的内部冷却通道。本研究调查的各种配置为平滑通道,具有90?横向肋骨和带有V形肋骨的通道成45°角。俯仰高度比(P / e),肋骨高度与液压直径之比(e / Dh)和纵横比(W / e)分别保持在12、0.1906和1。测试该配置的雷诺数范围为7,000到40,000。 45?发现肋产生最大的热传递和最小的压力损失。

著录项

  • 作者

    Subramanian Karthik;

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  • 年度 2006
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