TY - JOUR
T1 - Assessment of a novel k–ω turbulence model for transonic centrifugal impeller simulations
AU - Liu, Zhiyuan
AU - Wang, Peng
AU - Zhao, Ben
AU - Yang, Ce
N1 - Publisher Copyright:
© 2022 The Author(s).
PY - 2022/9
Y1 - 2022/9
N2 - Numerical simulation of high pressure ratio transonic centrifugal compressors is challenging for the existing turbulence models. A lagged k–ω model proposed by Olsen and Coakley for nonequilibrium effects was first applied to simulate the transonic centrifugal impeller SRV2-O. As comparative case studies, four other turbulence models (k–ω model, RNG k–ε model, SST-CC model, and EARSM model) were also computed. The comparison showed that (i) the selection of the turbulence model had a great influence on SRV2-O impeller simulations; (ii) the lagged k–ω model had an advantage over other models in terms of overall pressure ratio and internal flow characteristics; and (iii) the lagged model predicted a smaller blockage area caused by leakage vortex breakdown than other models, closer to the experimental result. The detailed parameter examination indicated that the nonequilibrium parameter a0 in the lagged model had little influence on the Mach number distribution and choking mass flow rate but a significant influence on the static pressure on the shroud casing. For a higher Mach number compressor, a smaller a0 is recommended for bettering the simulation accuracy.
AB - Numerical simulation of high pressure ratio transonic centrifugal compressors is challenging for the existing turbulence models. A lagged k–ω model proposed by Olsen and Coakley for nonequilibrium effects was first applied to simulate the transonic centrifugal impeller SRV2-O. As comparative case studies, four other turbulence models (k–ω model, RNG k–ε model, SST-CC model, and EARSM model) were also computed. The comparison showed that (i) the selection of the turbulence model had a great influence on SRV2-O impeller simulations; (ii) the lagged k–ω model had an advantage over other models in terms of overall pressure ratio and internal flow characteristics; and (iii) the lagged model predicted a smaller blockage area caused by leakage vortex breakdown than other models, closer to the experimental result. The detailed parameter examination indicated that the nonequilibrium parameter a0 in the lagged model had little influence on the Mach number distribution and choking mass flow rate but a significant influence on the static pressure on the shroud casing. For a higher Mach number compressor, a smaller a0 is recommended for bettering the simulation accuracy.
KW - transonic centrifugal compressor
KW - turbomachinery simulation
KW - turbulence model
UR - https://www.scopus.com/pages/publications/85138798559
U2 - 10.1139/tcsme-2021-0159
DO - 10.1139/tcsme-2021-0159
M3 - Article
AN - SCOPUS:85138798559
SN - 0315-8977
VL - 46
SP - 587
EP - 601
JO - Transactions of the Canadian Society for Mechanical Engineering
JF - Transactions of the Canadian Society for Mechanical Engineering
IS - 3
ER -