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STEADY AND UNSTEADY SIMULATION OF THE FLOW INSIDE A CENTRIFUGAL COMPRESSOR STAGE

机译:离心式压缩机级内流量的稳定和不稳定的模拟

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Computational investigations on a centrifugal compressor stage are presented to study unsteady interaction flow between the impeller and its vaned diffuser. Unsteady and steady calculations are compared with the measurement at different positions inside the diffuser. The influence of the impeller-diffuser interaction on the flow fields is discussed. Results show that qualitative and quite fair quantitative agreements are achieved between the unsteady predicted and measured flow fields. The interaction between the impeller and vaned diffuser can significantly change the calculated static pressure ratio and isentropic efficiency. The analysis shows that the unsteady interaction induces great change for the pressure on the diffuser vane and inlet flow condition and weakens quickly as radial increasing.
机译:提出了对离心式压缩机阶段的计算研究,以研究叶轮和叶片扩散器之间的不稳定相互作用。将不稳定和稳定的计算与扩散器内部不同位置的测量进行了比较。讨论了叶轮扩散器相互作用对流场的影响。结果表明,在不稳定的预测和测量的流场之间实现了定性和相当公平的定量协议。叶轮和叶片扩散器之间的相互作用可以显着改变计算的静压比和等熵效率。分析表明,不稳定的相互作用对扩散器叶片和入口流动条件的压力引起了大的变化,并且随着径向增加而削弱。

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