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Effect of expansion angle on turbulent swirling flow

机译:膨胀角对湍流涡流的影响

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摘要

This paper presents the numerical study ofswirling turbulent flow through different expansionangles which have many practical applications in gasturbines, combustors, etc. The governing differentialequations, which corporate k-#epsilon# turbulencemodel closure, are solved by a control-volume basediterative finite difference technique. Predicteddistribution for the mean velocities, turbulencekinetic energy and streamline plots are presented.Computations are done for different swirl numbers upto 1.5 and for different expansion angles between 30deg and 9O deg. With the increase of swirl strength,secondary on-axis recalculation is observed inaddition to the primary corner recalculation. Swirlproduces larger turbulence kinetic energy andenhances mixing rate, thus requiring shortercombustor length. For any particular swirl strengthbeyond the transition value, at smaller expansionangle, higher turbulence kinetic energy generationand consequently better mixing is found. The computedresults have been found to be comparable to the available experimental data.
机译:本文对通过不同膨胀角的涡流湍流进行了数值研究,这些湍流在燃气轮机、燃烧室等中具有许多实际应用。企业 k-#epsilon# 湍流模型闭合的控制微分方程通过基于控制体积的迭代有限差分技术求解。给出了平均速度、湍流动能和流线图的预测分布。计算高达1.5的不同漩涡数和30°g至9O°之间的不同膨胀角。随着漩涡强度的增加,除了一次拐角重计算外,还观察到二次轴上重计算。漩涡产生较大的湍流动能并提高混合速率,因此需要更短的燃烧室长度。对于任何特定的旋流强度超过过渡值,在较小的膨胀角下,产生更高的湍流动能,从而找到更好的混合。已发现计算结果与现有实验数据相当。

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