2020
DOI: 10.3390/app10062087
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Numerical Investigation on Aerodynamic Performance of SCO2 and Air Radial-Inflow Turbines with Different Solidity Structures

Abstract: Featured Application: This work can provide the design reference of rotor solidity for SCO 2 and air radial-inflow turbines as well as a new splitter structure to improve the performance of low solidity case. Abstract: Supercritical carbon dioxide (SCO 2 ) is of great use in miniature power systems. It obtains the characteristics of high density and low viscosity, which makes it possible to build a compact structure for turbomachinery. For a turbine design, an important issue is to figure out the appropriate s… Show more

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Cited by 9 publications
(5 citation statements)
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References 32 publications
(35 reference statements)
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“…The decrease in temperature has the least impact on the maximum leading edge diameter. Wang et al introduced the aerodynamic performance of radial inflow turbines with S-CO2 and air as working fluid considering different solidity, and provided design references for them [83]. In view of the low solidity of the S-CO2 turbine, a new diverter structure is proposed to improve its performance.…”
Section: Flow Characteristics Of S-co2 Turbinesmentioning
confidence: 99%
“…The decrease in temperature has the least impact on the maximum leading edge diameter. Wang et al introduced the aerodynamic performance of radial inflow turbines with S-CO2 and air as working fluid considering different solidity, and provided design references for them [83]. In view of the low solidity of the S-CO2 turbine, a new diverter structure is proposed to improve its performance.…”
Section: Flow Characteristics Of S-co2 Turbinesmentioning
confidence: 99%
“…High-quality hexahedral meshes are generated for each sample automatically through ANSYS TurboGrid software, where the wall regions are densely generated to satisfied the y + recommended by the turbulence model. The gridindependence verification is conducted and passed, and the results have been published in our previous work with the same turbine model and mesh generation setup (Wang et al, 2020). The simulation cases are then fed into ANSYS CFX software for simulation by Reynolds Average Navier-Stokes (RANS) method.…”
Section: Data Preparation Processmentioning
confidence: 99%
“…The simulation cases are then fed into ANSYS CFX software for simulation by Reynolds Average Navier-Stokes (RANS) method. According to our previous research (Wang et al, 2020), SST k-ω turbulence model is chosen so that more accurate result can be acquired. To be mentioned, the mesh around the hub, shroud and blade are more densely generated to fit the turbulence model (see Fig.…”
Section: Data Preparation Processmentioning
confidence: 99%
“…The programme NIST REFPROP has been cited widely throughout the literature for defining the thermodynamic and transport properties in sCO 2 turbomachinery design tools [14][15][16][17]. It provides thermophysical properties of pure and compound fluids over a broad range of states for liquids, gases and supercritical phases based on validated data and calculation methods.…”
Section: Meanline Designmentioning
confidence: 99%