首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >NUMERICAL COMPUTATION OF THE PERFORMANCE MAP OF A SUPERCRITICAL CO_2 RADIAL COMPRESSOR BY MEANS OF THREE-DIMENSIONAL CFD SIMULATIONS
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NUMERICAL COMPUTATION OF THE PERFORMANCE MAP OF A SUPERCRITICAL CO_2 RADIAL COMPRESSOR BY MEANS OF THREE-DIMENSIONAL CFD SIMULATIONS

机译:三维CFD仿真手段对超临界CO_2径向压缩机性能图的数值计算

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The performance map of a radial compressor operating with supercritical CO_2 is numerically computed by means of three dimensional stead]/ state Reynolds-averaged Navier-Stokes simulations. The results concern a 250 kW prototype. An in-house fluid dynamic solver is coupled with a thermodynamic library which ensures the highest accuracy of the thermophysical properties evaluation. Look-up table interpolation is used in order to reduce the computational cost, while keeping the desired level of accuracy in the fluid characterization. The compressor map is calculated considering three different rotational speeds (45 krpm, 50 krpm, and 55 krpm). For each speed-line several mass flow rates are simulated. Numerical results are compared to experimental data to prove the potential of the methodology.
机译:通过三维稳态/状态雷诺平均Navier-Stokes模拟,数值计算了超临界CO_2运行的径向压缩机的性能图。结果涉及一个250 kW的原型。内部流体动力学求解器与热力学库相结合,可确保热物理性质评估的最高准确性。使用查找表内插法来减少计算成本,同时在流体表征中保持所需的精确度。在考虑三个不同的转速(45 krpm,50 krpm和55 krpm)的情况下计算出压缩机特性图。对于每条速度线,都模拟了几个质量流率。将数值结果与实验数据进行比较,以证明该方法的潜力。

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