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Effect of high negative incidence on the performance of a centrifugal compressor stage with conventional vaned diffusers
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作者 ahti jaatinen Aki Grnman +1 位作者 Teemu Turunen-Saaresti Jari Backman 《Journal of Thermal Science》 SCIE EI CAS CSCD 2011年第2期97-105,共9页
Three vaned diffusers, designed to have high negative incidence (-8°) at the design operating point, are studied experimentally. The overall performance (efficiency and pressure ratio) are measured at three rotat... Three vaned diffusers, designed to have high negative incidence (-8°) at the design operating point, are studied experimentally. The overall performance (efficiency and pressure ratio) are measured at three rotational speeds, and flow angles before and after the diffuser are measured at the design rotational speed and with three mass flow rates. The results are compared to corresponding results of the original vaneless diffuser design. Attention is paid to the performance at lower mass flows than the design mass flow. The results show that it is possible to improve the performance at mass flows lower than the design mass flow with a vaned diffuser designed with high negative incidence. However, with the vaned diffusers, the compressor still stalls at higher mass flow rates than with the vaneless one. The flow angle distributions after the diffuser are more uniform with the vaned diffusers. 展开更多
关键词 centrifugal compressor vaned diffuser efficiency PERFORMANCE flow field
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Numerical Modelling of a Supersonic Axial Turbine Stator
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作者 Aki Grnman Teemu Turunen-Saaresti +1 位作者 ahti jaatinen Jari Backman 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第3期211-217,共7页
In order to improve the turbocharging process,a supersonic axial turbine stator was modelled numerically with a pulsatile inlet mass flow.The main objectives of the study were to find out how pulsation affects the flo... In order to improve the turbocharging process,a supersonic axial turbine stator was modelled numerically with a pulsatile inlet mass flow.The main objectives of the study were to find out how pulsation affects the flow field and the performance of the stator.At the beginning of the study,a supersonic turbine stator was modelled using three different techniques:quasi-steady,time-accurate with constant boundary conditions and time-accurate with a pulsatile inlet mass flow.The time-averaged and quasi-steady flow fields and performance were compared,and the flow field and stator performance with a pulsatile inlet mass flow was studied in detail at different time-steps.A hysteresis-like behaviour was captured when the total-to-static pressure ratio and efficiency were plotted as a function of the inlet mass flow over one pulse period.The total-to-static pressure ratio and efficiency followed the sinusoidal shape of the inlet flow as a function of time.It was also concluded that the stator efficiency decreases downstream from the stator trailing edge and the amplitude of the pulsating mass flow is decreased at the stator throat. 展开更多
关键词 CFD SUPERSONIC TURBINE STATOR TURBOCHARGING
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