TY - GEN
T1 - Optimization of an implicit LES method for underresolved simulations of incompressible flows
AU - Schranner, Felix S.
AU - Rozov, Vladyslav
AU - Adams, Nikolaus A.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - In engineering applications resolution, even within complex flow regions, is often low. In these underresolved regions, the truncation error of the underlying numerical schemes strongly affects the solution. If the truncation error functions as a physically consistent subgrid-scale (SGS) model, i.e. it models the evolution of otherwise resolved scales, resolution may be kept low. Thereby, computational efficiency is improved. The truncation error of high-order WENO-based schemes can function as an implicit subgrid-scale (SGS) model. The sixth-order adaptive central-upwind weighted essentially non-oscillatory scheme with implicit scale-separation, denoted as WENO-CU6-M1, potentially allows for physically consistent implicit SGS modeling, when shaped accordingly. In this work, finding an optimal formulation of WENO-CU6-M1 is considered within a deterministic design optimization framework. Possible surrogate modeling and sampling strategies are evaluated for their applicability. Design optimization bases on evaluation of a WENO-CU6-M1 formulation’s potential to reproduce Kolmogorov scaling for a TaylorGreen vortex flow in its quasi-isotropic state. As in the absence of physical viscosity, kinetic-energy dissipates exclusively due to SGS, the Reynolds number is infinite and the evolution of the flow is determined by proper SGS modeling. To complete the work, we quantify the effective numerical dissipation rate of the WENO-CU6-M1 model optimized for artificially compressible fluid flows and compare it to the original one.
AB - In engineering applications resolution, even within complex flow regions, is often low. In these underresolved regions, the truncation error of the underlying numerical schemes strongly affects the solution. If the truncation error functions as a physically consistent subgrid-scale (SGS) model, i.e. it models the evolution of otherwise resolved scales, resolution may be kept low. Thereby, computational efficiency is improved. The truncation error of high-order WENO-based schemes can function as an implicit subgrid-scale (SGS) model. The sixth-order adaptive central-upwind weighted essentially non-oscillatory scheme with implicit scale-separation, denoted as WENO-CU6-M1, potentially allows for physically consistent implicit SGS modeling, when shaped accordingly. In this work, finding an optimal formulation of WENO-CU6-M1 is considered within a deterministic design optimization framework. Possible surrogate modeling and sampling strategies are evaluated for their applicability. Design optimization bases on evaluation of a WENO-CU6-M1 formulation’s potential to reproduce Kolmogorov scaling for a TaylorGreen vortex flow in its quasi-isotropic state. As in the absence of physical viscosity, kinetic-energy dissipates exclusively due to SGS, the Reynolds number is infinite and the evolution of the flow is determined by proper SGS modeling. To complete the work, we quantify the effective numerical dissipation rate of the WENO-CU6-M1 model optimized for artificially compressible fluid flows and compare it to the original one.
UR - http://www.scopus.com/inward/record.url?scp=85007549055&partnerID=8YFLogxK
U2 - 10.2514/6.2016-0338
DO - 10.2514/6.2016-0338
M3 - Conference contribution
AN - SCOPUS:85007549055
SN - 9781624103933
T3 - 54th AIAA Aerospace Sciences Meeting
BT - 54th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA Aerospace Sciences Meeting, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -