TY - JOUR
T1 - Comparison of computation models for simulation of turbomachinery rotor-stator interactions
AU - Du, Peng Cheng
AU - Ning, Fang Fei
N1 - Publisher Copyright:
© 2017, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2017/3/1
Y1 - 2017/3/1
N2 - Comparative study on three Fourier-based time-domain unsteady computation methods, including the shape-correction phase shift method, space-time gradient method and harmonic balance method, was carried out by simulation of two typical kinds of rotor-stator interactions, i.e.: wake-blade interactions and shock-blade interactions. Differences and relations between these computation methods were investigated in detail, and their computational accuracy and speed were also analyzed. The results indicate that three methods can resolve the unsteady flow details well. Compared with the conventional time-marching method, the computational speed of these methods can be enhanced from several to dozens of times, making these methods applicable to daily design process.
AB - Comparative study on three Fourier-based time-domain unsteady computation methods, including the shape-correction phase shift method, space-time gradient method and harmonic balance method, was carried out by simulation of two typical kinds of rotor-stator interactions, i.e.: wake-blade interactions and shock-blade interactions. Differences and relations between these computation methods were investigated in detail, and their computational accuracy and speed were also analyzed. The results indicate that three methods can resolve the unsteady flow details well. Compared with the conventional time-marching method, the computational speed of these methods can be enhanced from several to dozens of times, making these methods applicable to daily design process.
KW - Harmonic balance method
KW - Rotor-stator interactions
KW - Shape-correction phase shift method
KW - Space-time gradient method
KW - Turbomachinery
UR - https://www.scopus.com/pages/publications/85019748772
U2 - 10.13224/j.cnki.jasp.2017.03.003
DO - 10.13224/j.cnki.jasp.2017.03.003
M3 - 文章
AN - SCOPUS:85019748772
SN - 1000-8055
VL - 32
SP - 528
EP - 537
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 3
ER -