2021
DOI: 10.1016/j.matcom.2020.09.010
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Introducing compressibility with SIMPLE algorithm

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Cited by 10 publications
(5 citation statements)
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“…The conservation equations are solved by using iterative methods, and the linear upwind differencing scheme is employed. The SIMPLE algorithm is implemented to couple the equations for velocity and pressure governing mass and momentum conservation. , To improve solution convergence, under-relaxation is used. The solution converges to within an absolute tolerance of 10 –6 .…”
Section: Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…The conservation equations are solved by using iterative methods, and the linear upwind differencing scheme is employed. The SIMPLE algorithm is implemented to couple the equations for velocity and pressure governing mass and momentum conservation. , To improve solution convergence, under-relaxation is used. The solution converges to within an absolute tolerance of 10 –6 .…”
Section: Methodsmentioning
confidence: 99%
“…The SIMPLE algorithm is implemented to couple the equations for velocity and pressure governing mass and momentum conservation. 71,72 To improve solution convergence, under-relaxation is used. The solution converges to within an absolute tolerance of 10 −6 .…”
Section: Geometry and Meshingmentioning
confidence: 99%
“…The governing equations were discretized on unstructured, nested, Cartesian‐like grids. The Navier‐Stokes equations were advanced in time using a Semi‐Implicit Method for Pressure Linked Equations (SIMPLE) algorithm in which an intermediate velocity is calculated by solving the momentum equations without the pressure term and then the final velocity is obtained using a pressure correction that ensures the continuity equation is satisfied (Patankar & Spalding, 1972; Qin et al., 2021; Xu et al., 2022). The convection terms in the momentum equations were discretized using a Hybrid‐Bounded central difference scheme, which couples a higher‐order upwind scheme in regions where the RANS mode is active with a bounded central difference scheme in regions where the LES mode is active.…”
Section: Test Cases Computational Approach and Model Validationmentioning
confidence: 99%
“…R1 was used, and the finite volume method was used to discretize the governing equations. The pressure field and velocity field were considered in terms of coupling and computation time, and the SIMPLE algorithm was applied [43]. The spatial discretization of momentum and energy was set to quadratic.…”
Section: Geometry and Boundary Conditionsmentioning
confidence: 99%