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Analysis on the unsteady flow structures in the tip region of axial compressor

机译:轴向压缩机尖端区域的不稳定流动结构分析

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The unsteady characteristic in the tip region of an axial compressor has been numerically studied with the help of the dynamic mode decomposition analysis. The characteristics of frequency and dynamic modes are compared and discussed under different operating points and different parameters, such as tip clearance and rotating speeds. For the flowfield structures in the tip region, such as tip leakage flow, separation flow and shock wave, their relationships with the unsteadiness are studied in detail. Except for the unsteadiness caused by the interaction between rotating rotor and the stationary boundaries, it is found that the unsteadiness is attributed to the moving of the low-velocity cell. Based on the generation and the development of the low-velocity cell, the unsteady characteristics in tip region are divided into 4 types: BPF-dominated, shedding-dominated, self-induced and separation-dominated. When the tip leakage flow is weak, the unsteadiness in the tip region is only triggered by the blade sweeping. As the tip leakage flow gets stronger to a certain extent, the low-velocity cell is shed into the flow passage and mixed with the main-flow. When the main-flow is weaker under the low flowrate condition, the interaction between the low-velocity cell and the pressure side occurs and generates a new low-velocity cell near the leading-edge of the neighboring blade. The frequency of the new cell generation is actually the self-induced frequency. In the zero and small clearance model, the low-velocity is shed by the separation in the leading-edge and the casing-suction corner. By understanding these unsteady characteristics, the change tendency of the leading frequency in the rotor tip is easily explained and forecasted. Furthermore, under the transonic operation condition, the low-velocity cell is decelerated and eliminated by the shock wave in the unsteadiness of the self-induced type and the separation-dominated type, respectively. Thus, the leading frequency in the tip flow field is moderated.
机译:轴向压缩机的尖端区域中的不稳定特性已经在动态模式分解分析的帮助下进行了数值研究。比较频率和动态模式的特性,并在不同的操作点和不同的参数下讨论,例如尖端间隙和旋转速度。对于尖端区域中的流场结构,例如尖端泄漏流动,分离流动和冲击波,详细研究了它们与不稳定性的关系。除了由旋转转子与静止边界之间的相互作用引起的不稳定性,发现不稳定归因于低速电池的移动。基于低速细胞的产生和发展,尖端区域的不稳定特性分为4种类型:BPF主导,脱落主导,自我诱导和分离主导地位。当尖端泄漏流弱时,尖端区域中的不稳定性仅被刀片扫描触发。由于尖端泄漏流动在一定程度上变得更强,因此低速电池被缩进到流动通道中并与主流混合。当主流在低流量条件下较弱时,低速电池和压力侧之间的相互作用发生并在相邻叶片的前缘附近产生新的低速单元。新的小区生成的频率实际上是自诱导的频率。在零和小的间隙模型中,低速通过前缘和壳体抽吸角中的分离脱落。通过了解这些不稳定的特性,容易解释和预测转子尖端中的前导频率的变化趋势。此外,在跨型操作条件下,分别在自诱导类型和分离主导型不稳定的冲击波中减速和消除低速电池。因此,尖端流场中的前导频率被调节。

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