Advances of Computational Fluid Dynamics in Nuclear Reactor Design and Safety Assessment 2019
DOI: 10.1016/b978-0-08-102337-2.00002-x
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Computational fluid dynamics

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Cited by 27 publications
(21 citation statements)
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“…Furthermore, Courant-Friedrich-Levy (CFL) condition is satisfied in resolving the time scale. 64 The time step size is determined using Equation (39) to make it small enough to be consistent with the fine mesh size, where Δt, CFL, Δx, and U represent the time step, CFL number, minimum grid size, and the velocity, respectively.…”
Section: Meshing and Model Validationmentioning
confidence: 99%
See 1 more Smart Citation
“…Furthermore, Courant-Friedrich-Levy (CFL) condition is satisfied in resolving the time scale. 64 The time step size is determined using Equation (39) to make it small enough to be consistent with the fine mesh size, where Δt, CFL, Δx, and U represent the time step, CFL number, minimum grid size, and the velocity, respectively.…”
Section: Meshing and Model Validationmentioning
confidence: 99%
“…The numerical case is prepared in such a way that the computational domain is large enough to accommodate the large eddies of interest. Furthermore, Courant–Friedrich–Levy (CFL) condition is satisfied in resolving the time scale 64 . The time step size is determined using Equation () to make it small enough to be consistent with the fine mesh size, where italicΔt, italicCFL, italicΔx, and U represent the time step, CFL number, minimum grid size, and the velocity, respectively. italicΔtgoodbreak=italicCFL*italicΔxU0.25em …”
Section: Meshing and Model Validationmentioning
confidence: 99%
“…at numerous node points of the mesh. With appropriate boundary conditions, it is possible to solve these equations iteratively for the flow field variables at each computational point …”
Section: Mathematical Modelsmentioning
confidence: 99%
“…The governing equations listed above are solved using Fluent 18.0 with a finite volume code with the steady-state approximation. The SIMPLE (semi-implicit pressure linked equation) algorithm is adopted for pressure–velocity coupling . The second-order upwind scheme has been adopted for discretization.…”
Section: Cfd Modelingmentioning
confidence: 99%