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Application of Super-Computer Technologies in the Research and Improvement of Steps and Elements of the Flow Path of the Turbocompressors

机译:超级计算机技术在涡轮机的流动路径的研究和改进研究和改进中的应用

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This paper presents the results of the study of the spatial flow in the turbocompressors elements of computational fluid dynamics methods using the Ansys CFX software package on a multiprocessor computer system. Five objects of research are considered: 1) flow path of an intermediate stage of an average-flow centrifugal compressor; 2) flow path of the low-flow centrifugal compressor stage; 3) a natural gas centrifugal compressor stage; 4) vaned diffuser of the first stage of an industrial multistage centrifugal compressor; 5) adjustable inlet stator of the first stage of an industrial turbocompressors. Generally at manufacturing new centrifugal compressors, it is impossible to make a control measurement of the parameters of the working process inside the flow path elements. Computational fluid dynamics methods are widely used to overcome this difficulties. However verification and validation of CFD methods are necessary for accurate modeling of the workflow. All calculations were performed on one of the SPbPU clusters. Parameters of one cluster: AMD Opteron 280 4 cores. The calculations were carried out with parallel running of the processors: HP MPI Distributed Parallel and HP MPI Local Parallel for different objects.
机译:本文介绍了使用多处理器计算机系统上的ANSYS CFX软件包的计算流体动力学方法的涡轮机动力学方法中空间流量的研究结果。五个研究对象被认为是:1)平均流动离心压缩机的中间级的流动路径; 2)低流量离心压缩机级的流动路径; 3)天然气离心式压缩机级; 4)工业多级离心式压缩机第一级的叶片扩散器; 5)工业涡轮机的第一阶段的可调节入口定子。通常在制造新的离心式压缩机时,不可能对流路元件内的工作过程的参数进行控制测量。计算流体动力学方法广泛用于克服这种困难。但是,CFD方法的验证和验证是准确的工作流程建模所必需的。在其中一个SPBPU集群上进行所有计算。一个集群的参数:AMD Opteron 280 4核心。使用处理器的并行运行执行计算:HP MPI分布并行和HP MPI局部并行针对不同的对象。

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