2010
DOI: 10.1016/j.compfluid.2010.02.002
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Large-scale DES computations of the forward speed diffraction and pitch and heave problems for a surface combatant

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Cited by 63 publications
(34 citation statements)
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“…Dynamic overset grids are used to solve grid deformations and relative motions [30], with the interpolation coefficients between the grids recomputed dynamically at run time with the code Suggar [31]. Large-scale computations are achieved using high performance computing (HPC) with an MPI-based domain decomposition approach [32]. For complete details the reader is referred to the references [28e30,32] and literature therein.…”
Section: Flow Solvermentioning
confidence: 99%
“…Dynamic overset grids are used to solve grid deformations and relative motions [30], with the interpolation coefficients between the grids recomputed dynamically at run time with the code Suggar [31]. Large-scale computations are achieved using high performance computing (HPC) with an MPI-based domain decomposition approach [32]. For complete details the reader is referred to the references [28e30,32] and literature therein.…”
Section: Flow Solvermentioning
confidence: 99%
“…1 Coupling of flow, overset, and propeller solvers. Overset connectivity solver is shown as single-lagged, explicit; other configurations are described in Carrica et al (2010) allowed to vary in all spatial directions, but is frozen in time. A drag coefficient is used to model viscous forces on the blades.…”
Section: Propeller Modelingmentioning
confidence: 99%
“…The current architecture of the coupled code also runs Suggar in multiple lagged mode, as described in detail in Carrica et al (2010). This is shown in Fig.…”
Section: Coupling Of Flow and Propeller Solversmentioning
confidence: 99%
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“…This program was also validated by Guo et al (2012) for calculating the added resistance of KVLCC2 type hulls in head waves. Recently, Sadat-Hosseini et al (2013) presented the added resistance calculation of KVLCC2 by both experiment and numerical method using CFDShip-Iowa v4.5 (Carrica et al, 2010), which is an overset, block structured CFD solver with RANS and DES for turbulence modeling and a singlephase level-set method for free-surface capturing.…”
Section: Introductionmentioning
confidence: 99%