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首页> 外文期刊>International Journal of Turbo and Jet Engines >Direct Numerical Simulation of Turbine Cascade Flow with Heat Transfer
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Direct Numerical Simulation of Turbine Cascade Flow with Heat Transfer

机译:热传递汽轮机级联流动的直接数值模拟

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摘要

Two- and three-dimensional direct numerical simulation (DNS) of turbine cascade flow at low Reynolds number with heat transfer are performed using high-order finite difference method. Two-dimensional laminar computation which is used to construct the initial flow of three-dimensional DNS fails to predict Stanton number on the second half of suction side where the flow is turbulent in experiment. In three-dimensional DNS, transition is triggered by periodic blow-and-suction disturbances. Numerical experiments show that phase randomness of the disturbance is not necessary to trigger the transition which can be induced by disturbances with fixed phases. In a range of time fundamental frequency of disturbance, when increasing the frequency, transition moves downstream. When time fundamental frequency is big enough, transition disappears. With fixed space phases, time phases and selected time fundamental frequency, time averaged pressure and Stanton number distributions of three-dimensional DNS coincide with the experimental datum. Averaged velocity and temperature, Root-Mean-squares (RMS) of velocity pulse,temperature pulse, Reynolds shear stress and heat flux are extracted from the DNS database. All statistics agree well with experimental and theoretical results which verify the accuracy of present database.
机译:使用高阶有限差分法执行具有传热的低雷诺数的涡轮机级联流动的两维和三维直接数值模拟(DNS)。用于构造三维DNS的初始流动的二维层状计算不能预测吸入侧的第二半部分上的斯坦顿数,其中流动在实验中是湍流的。在三维DNS中,过渡通过周期性的吹气干扰触发。数值实验表明,扰动的相随机性是不需要触发可以通过固定相的干扰引起的过渡。在扰动的一系列基本频率下,在增加频率时,转换在下游移动。当时间基频足够大时,过渡消失。利用固定空间阶段,时间阶段和选定的时代频率,三维DNS的时间平均压力和Stanton数分布与实验性数据相一致。从DNS数据库中提取平均速度和温度,温度脉冲,雷诺剪切应力和热通量的速度脉冲,温度脉冲,雷诺平方体(RMS)。所有统计数据都与实验和理论结果一致,验证了当前数据库的准确性。

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