TY - GEN
T1 - Numerial simulation of incipient rotating stall characteristics in a mixed-flow pump
AU - Li, Wei
AU - Agarwal, Ramesh K.
AU - Ji, Leilei
AU - Li, Enda
AU - Zhou, Ling
N1 - Funding Information:
This work was sponsored by the National Natural Science Foundation of China (No.51679111, No.51409127 and No.51579118), National Key R&D Program Project (No.2017YFC0403703), PAPD, Natural Science Foundation of Jiangsu Province (No.BK20161472, No.BK20160521).
Publisher Copyright:
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Rotating stall is an unstable phenomenon, which has an important influence on the performance of a mixed-flow pump. In this paper, the internal flow characteristics and the energy performance of a mixed-flow pump in incepient stall condition are numerically simulated using three turbulence models, namely the standard k-ε, k-ω and SST k-ω. The numerical results are analyzed and compared with the experimental results from an energy performance test and Particle Image Velocimetry (PIV). The analysis of the results shows that the turbulence models have significant influence on predicting the stall characteristics. The hump zone calculated by the SST k-ω turbulence model is more obvious than that obtained by using the k-ε and k-ω models; however the flow rate condition at the lowest point of the hump zone has little difference in the results from various turbulence models. The simulations with SST k-ω model can better capture the stall vortex and separated flow in the mixed-flow pump compared to the other two models. Furthermore, the efficiency of the pump and stall flow field predicted by the SST k-ω model gives the best agreement with the experiment data.
AB - Rotating stall is an unstable phenomenon, which has an important influence on the performance of a mixed-flow pump. In this paper, the internal flow characteristics and the energy performance of a mixed-flow pump in incepient stall condition are numerically simulated using three turbulence models, namely the standard k-ε, k-ω and SST k-ω. The numerical results are analyzed and compared with the experimental results from an energy performance test and Particle Image Velocimetry (PIV). The analysis of the results shows that the turbulence models have significant influence on predicting the stall characteristics. The hump zone calculated by the SST k-ω turbulence model is more obvious than that obtained by using the k-ε and k-ω models; however the flow rate condition at the lowest point of the hump zone has little difference in the results from various turbulence models. The simulations with SST k-ω model can better capture the stall vortex and separated flow in the mixed-flow pump compared to the other two models. Furthermore, the efficiency of the pump and stall flow field predicted by the SST k-ω model gives the best agreement with the experiment data.
UR - http://www.scopus.com/inward/record.url?scp=85083942138&partnerID=8YFLogxK
U2 - 10.2514/6.2019-2314
DO - 10.2514/6.2019-2314
M3 - Conference contribution
AN - SCOPUS:85083942138
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -