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AVERAGE PASSAGE FLOW FIELD AND DETERMINISTIC STRESSES IN THE TIP AND HUB REGIONS OF A MULTI-STAGE TURBOMACHINE

机译:多级涡轮机的尖端和轮毂区域的平均通道流场和确定的应力

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This paper continues our effort to study the dynamics of deterministic stresses in a multistage turbomachine using experimental data. Here we focus on the tip .and hub regions and compare them to mid span data obtained in previous studies. The analysis is based on data obtained in PIV measurements performed in the second stage of a two-stage turbomachine. A complete data set is obtained using blades and fluid with matched optical index of refraction. Previous measurements at mid span have shown that at mid span and close to design conditions, the deterministic kinetic energy is smaller than the turbulent kinetic energy. The primary contributor to the deterministic stresses at mid span is the interaction of a blade with the upstream wakes. Conversely, we find that the tip vortex is the dominant source of phase-dependent unsteadiness and deterministic stresses in the tip region. Along the trajectory of the tip vortex, the deterministic kinetic energy levels are more than one order of magnitude higher than the levels measured in the hub and mid-span, and are of the same order of magnitude as the turbulent kinetic energy levels. Reasons for this trend are explained using a sample distribution of phase-averaged flow variables. Outside of the region affected by tip vortex transport, within the rotor-stator gap and within the stator passages, the turbulent kinetic energy is still 3-4 times higher than the deterministic kinetic energy. The deterministic and turbulent shear stress levels are comparable in all spanwise locations, except for the wakes of the stator blades, where the turbulent stresses are higher. However, along the direction of tip vortex transport, the deterministic shear stresses are about an order of magnitude higher than the turbulent shear stresses. The decay rates of deterministic kinetic energy in the hub and mid-span regions are comparable to each other, whereas at the tip, the decay rate is higher. The decay rates of turbulent kinetic energy are much smaller than those of the deterministic kinetic energy. The paper also examines terms in the deterministic kinetic energy transport equation. The data indicate that "Deterministic Production" and a new term, called here "Dissipation due to Turbulence" are the dominant source/sink terms. Regions with alternating signs of Deterministic Production indicate that the energy transfer between the phase-averaged and average-passage flow fields can occur in both directions. The divergence of the Pressure-Velocity correlation, obtained from a balance of all the other terms, is dominant and appears to be much larger than the deterministic production (source/sink) term. This trend indicates that there are substantial deterministic pressure fluctuations in the flow field, especially within the rotor-stator gap and within the stator passage.
机译:本文继续我们的工作,使用实验数据研究多级涡轮机中确定性应力的动力学。在这里,我们将重点放在尖端和枢纽区域,并将它们与先前研究中获得的中跨数据进行比较。该分析基于在两级涡轮机的第二级中执行的PIV测量中获得的数据。使用具有匹配的光学折射率的叶片和流体可以获得完整的数据集。先前的中跨测量表明,在中跨和接近设计条件的情况下,确定性动能小于湍流动能。中间跨度确定性应力的主要来源是叶片与上游尾流的相互作用。相反,我们发现尖端涡旋是尖端区域中相变不稳定和确定性应力的主要来源。沿着尖端涡旋的轨迹,确定性动能水平比在轮毂和中跨中测得的水平高一个数量级,并且与湍流动能水平处于相同数量级。使用相位平均流量变量的样本分布来解释这种趋势的原因。在受尖端涡流传输影响的区域之外,在转子-定子间隙内以及在定子通道内,湍流动能仍比确定性动能高3-4倍。确定性和湍流剪切应力水平在所有翼展方向上都是可比的,除了静叶片的尾流(湍流应力较高)之外。然而,沿着尖端涡流传输的方向,确定性剪应力比湍流剪应力高大约一个数量级。轮毂和中跨区域中确定性动能的衰减率彼此可比,而在尖端,衰减率更高。湍动能的衰减率比确定性动能的衰减率小得多。本文还研究了确定性动能传输方程中的项。数据表明,“确定性生产”和一个新术语(此处称为“由于湍流引起的耗散”)是主要的源/汇术语。具有确定性生产交替符号的区域表明,相平均流场和平均通道流场之间的能量转移可以在两个方向上发生。从其他所有条件的平衡中得出的压力-速度相关性的差异占主导地位,并且似乎比确定性生产(源/汇)条件大得多。这种趋势表明,在流场中存在确定性的压力波动,尤其是在转子-定子间隙内和定子通道内。

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