Mathematical and Numerical Modeling of Turbulent Flows

被引:9
作者
Vedovoto, Joao M. [1 ]
Serfaty, Ricardo [2 ]
Neto, Aristeu da Silveira [1 ]
机构
[1] Univ Fed Uberlandia, Fac Engn Mecan, BR-38400902 Uberlandia, MG, Brazil
[2] CENPES PETROBRAS, BR-21941915 Rio De Janeiro, RJ, Brazil
来源
ANAIS DA ACADEMIA BRASILEIRA DE CIENCIAS | 2015年 / 87卷 / 02期
关键词
Turbulent flows; Large Eddy Simulation; Immersed Boundary Method; Low-Mach Number Flows; Industrial Flows; IMMERSED BOUNDARY METHOD; LARGE-EDDY SIMULATIONS; SUBGRID-SCALE MODEL; DYNAMICS;
D O I
10.1590/0001-3765201520140510
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
The present work is devoted to the development and implementation of a computational framework to perform numerical simulations of low Mach number turbulent flows over complex geometries. The algorithm under consideration is based on a classical predictor-corrector time integration scheme that employs a projection method for the momentum equations. The domain decomposition strategy is adopted for distributed computing, displaying very satisfactory levels of speed-up and efficiency. The Immersed Boundary Methodology is used to characterize the presence of a complex geometry. Such method demands two separate grids: An Eulerian, where the transport equations are solved with a Finite Volume, second order discretization and a Lagrangian domain, represented by a non-structured shell grid representing the immersed geometry. The in-house code developed was fully verified by the Method of Manufactured Solutions, in both Eulerian and Lagrangian domains. The capabilities of the resulting computational framework are illustrated on four distinct cases: a turbulent jet, the Poiseuille flow, as a matter of validation of the implemented Immersed Boundary methodology, the flow over a sphere covering a wide range of Reynolds numbers, and finally, with the intention of demonstrating the applicability of Large Eddy Simulations LES - in an industrial problem, the turbulent flow inside an industrial fan.
引用
收藏
页码:1195 / 1232
页数:38
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