Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method

Kazutoyo Yamada, Kazuya Kusano, Masato Furukawa

Research output: Contribution to conferencePaper

Abstract

Recently, the lattice Boltzmann method (LBM) is being applied in turbomachinery field, regarded as a good candidate for tool of flow simulation as well as aerodynamic sound analysis. For better prediction of broadband noise with high frequecy, which is generally generated in high Reynolds number flows, not only high grid resolution is required to capture very small eddies of the sound source inside the turbulent boundary layer, but also the computation of acoustic field is often needed. In such case, the direct simulation of flow field and acoustic field is straightforward and effective. However, the computational cost becomes extremely expensive. Moreover, for low Mach number flows the compressible Navier-Stokes simulation not only requires high-order scheme which is unsuitable for parallel computation, but also suffers from stiff problem. LBM is suitable for such simulation thanks to its advantages. In the present study, a large-scale numerical simulation of flow field around a half-ducted propeller fan is conducted with LBM, and its result is validated by comparing with the experimental result.

Original languageEnglish
DOIs
Publication statusPublished - Jan 1 2015
EventASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015 - Seoul, Korea, Republic of
Duration: Jul 26 2015Jul 31 2015

Other

OtherASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015
CountryKorea, Republic of
CitySeoul
Period7/26/157/31/15

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Acoustic fields
Propellers
Unsteady flow
Fans
Flow fields
Acoustic waves
Turbomachinery
Flow simulation
Computer simulation
Acoustic noise
Mach number
Aerodynamics
Boundary layers
Reynolds number
Costs

All Science Journal Classification (ASJC) codes

  • Fluid Flow and Transfer Processes

Cite this

Yamada, K., Kusano, K., & Furukawa, M. (2015). Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method. Paper presented at ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015, Seoul, Korea, Republic of. https://doi.org/10.1115/AJKFluids2015-09494

Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method. / Yamada, Kazutoyo; Kusano, Kazuya; Furukawa, Masato.

2015. Paper presented at ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015, Seoul, Korea, Republic of.

Research output: Contribution to conferencePaper

Yamada, K, Kusano, K & Furukawa, M 2015, 'Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method' Paper presented at ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015, Seoul, Korea, Republic of, 7/26/15 - 7/31/15, . https://doi.org/10.1115/AJKFluids2015-09494
Yamada K, Kusano K, Furukawa M. Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method. 2015. Paper presented at ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015, Seoul, Korea, Republic of. https://doi.org/10.1115/AJKFluids2015-09494
Yamada, Kazutoyo ; Kusano, Kazuya ; Furukawa, Masato. / Large-scale numerical simulation of unsteady flow field in a half-ducted propeller fan using lattice Boltzmann method. Paper presented at ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, AJKFluids 2015, Seoul, Korea, Republic of.
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