TY - CONF
T1 - Numerical prediction of noise from the internal flow in a centrifugal blower
AU - Guo, Yang
AU - Kato, Chisachi
AU - Yamade, Yoshinobu
AU - Ohta, Yutaka
AU - Iwase, Taku
AU - Takayama, Ryo
N1 - Funding Information:
This work was supported in part by the Ministry of Education, Culture, Sports, Science and Technology (MEXT), Japan under the High Performance Computing Infrastructure (HPCI) Strategic Program: "Field 4: Industrial Innovation". The authors would like to thank the members of the third working group of "HPC project for turbomachinery" for the useful discussion about CFD and CAA.
Publisher Copyright:
Copyright © 2015 by JSME.
PY - 2015
Y1 - 2015
N2 - The noise generated from the internal flow in a centrifugal blower was computed by computational aero-acoustics (CAA). The sound sources were obtained by computational fluid dynamics (CFD), using large-eddy simulation (LES) to compute the turbulent flow in the centrifugal blower. The computed sound pressure level (SPL) with sound source from coarse mesh LES is overpredicted, while the computed SPL with sound source from fine mesh LES agrees fairly well with the experimental data. The peak of SPL at blade passing frequency (BPF) of 600 Hz can be somewhat captured by CAA with sound source from fine mesh CFD. However, due to the short computational time, the frequency resolution is not fine in CAA with sound source from fine mesh CFD, which may be the reason of underprediction of the peak value at BPF. Fluid forces acting on the impeller at the plane perpendicular to the axial direction play important role on the predicted SPL at BPF.
AB - The noise generated from the internal flow in a centrifugal blower was computed by computational aero-acoustics (CAA). The sound sources were obtained by computational fluid dynamics (CFD), using large-eddy simulation (LES) to compute the turbulent flow in the centrifugal blower. The computed sound pressure level (SPL) with sound source from coarse mesh LES is overpredicted, while the computed SPL with sound source from fine mesh LES agrees fairly well with the experimental data. The peak of SPL at blade passing frequency (BPF) of 600 Hz can be somewhat captured by CAA with sound source from fine mesh CFD. However, due to the short computational time, the frequency resolution is not fine in CAA with sound source from fine mesh CFD, which may be the reason of underprediction of the peak value at BPF. Fluid forces acting on the impeller at the plane perpendicular to the axial direction play important role on the predicted SPL at BPF.
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U2 - 10.1115/AJKFluids2015-09194
DO - 10.1115/AJKFluids2015-09194
M3 - Paper
AN - SCOPUS:85044329224
T2 - ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015
Y2 - 26 July 2015 through 31 July 2015
ER -