TY - GEN
T1 - Unsteady turbulent flow simulation using lattice boltzmann method with near-wall modeling
AU - Maeyama, Hirotaka
AU - Imamura, Taro
AU - Osaka, Jun
AU - Kurimoto, Naoki
N1 - Funding Information:
This research was funded by JSPS KAKENHI Grant Number 19J12009 (Grant-in-Aid for JSPS Fellows). The calculations on this paper were conducted using the SGI Rackable C2112-4GP3/C1102-GP8 (Reedbush-U) in the Information Technology Center, The University of Tokyo.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - A novel wall-modeled large-eddy simulation (WMLES) based on lattice Boltzmann method (LBM) is presented. Near-wall modeling for a turbulent boundary layer is essential in order to calculate the high Reynolds number wall-bounded turbulent flow that appears in an actual engineering field. WMLES based on the reconstruction of distribution functions is further developed to handle the objects on a non-body-fitted Cartesian grid. In order to overcome the drawback of the existing model, Image-Point (IP) is introduced to the model. Furthermore, the strategy to determine the turbulent eddy viscosity profile near the wall is proposed by considering the shear-stress balance in an inner layer. For the validation of the proposed model, numerical simulations of a turbulent channel flow are conducted and the calculation results are compared with the DNS results or the semi-analytical profile in terms of the streamwise velocity and the resolved Reynolds shear stress profiles. The proposed model is observed to be both robust and accurate, yielding the very satisfactory results regardless of the angle between the Cartesian grid line and the wall.
AB - A novel wall-modeled large-eddy simulation (WMLES) based on lattice Boltzmann method (LBM) is presented. Near-wall modeling for a turbulent boundary layer is essential in order to calculate the high Reynolds number wall-bounded turbulent flow that appears in an actual engineering field. WMLES based on the reconstruction of distribution functions is further developed to handle the objects on a non-body-fitted Cartesian grid. In order to overcome the drawback of the existing model, Image-Point (IP) is introduced to the model. Furthermore, the strategy to determine the turbulent eddy viscosity profile near the wall is proposed by considering the shear-stress balance in an inner layer. For the validation of the proposed model, numerical simulations of a turbulent channel flow are conducted and the calculation results are compared with the DNS results or the semi-analytical profile in terms of the streamwise velocity and the resolved Reynolds shear stress profiles. The proposed model is observed to be both robust and accurate, yielding the very satisfactory results regardless of the angle between the Cartesian grid line and the wall.
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U2 - 10.2514/6.2020-2565
DO - 10.2514/6.2020-2565
M3 - Conference contribution
AN - SCOPUS:85092505811
SN - 9781624105982
T3 - AIAA AVIATION 2020 FORUM
BT - AIAA AVIATION 2020 FORUM
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA AVIATION 2020 FORUM
Y2 - 15 June 2020 through 19 June 2020
ER -