TY - JOUR
T1 - Investigation on distributed viscous body force modeling and its application
AU - Liu, Chao
AU - Ning, Fang Fei
PY - 2011/1
Y1 - 2011/1
N2 - The modeling method of viscous terms of Navier-Stokes equations using distributed viscous body forces was investigated. Then a fast calculation code for the three-dimensional(3-D) unsteady flow in turbomachine was developed, by solving 3-D unsteady Euler equations with the distributed viscous body force model. The code was used to simulate the unsteady flow in a two-stage compressor under circumferential total pressure inlet distortion, and the results were compared with Reynolds averaged Navier-Stokes(RANS) results. This demonstrates that, in the simulation of the unsteady flow in the multi-stage compressor under inlet distortion, the results obtained by the distributed viscous body force model agree well with the RANS results, with substantially less computational cost.
AB - The modeling method of viscous terms of Navier-Stokes equations using distributed viscous body forces was investigated. Then a fast calculation code for the three-dimensional(3-D) unsteady flow in turbomachine was developed, by solving 3-D unsteady Euler equations with the distributed viscous body force model. The code was used to simulate the unsteady flow in a two-stage compressor under circumferential total pressure inlet distortion, and the results were compared with Reynolds averaged Navier-Stokes(RANS) results. This demonstrates that, in the simulation of the unsteady flow in the multi-stage compressor under inlet distortion, the results obtained by the distributed viscous body force model agree well with the RANS results, with substantially less computational cost.
KW - Compressor stability
KW - Distributed viscous body force model
KW - Inlet distortion
KW - Multi-stage compressor
KW - Three-dimensional(3-D) unsteady flow
UR - https://www.scopus.com/pages/publications/79952463724
M3 - 文章
AN - SCOPUS:79952463724
SN - 1000-8055
VL - 26
SP - 128
EP - 135
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 1
ER -