2008
DOI: 10.1007/s00466-008-0276-0
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A nested iterative scheme for computation of incompressible flows in long domains

Abstract: We present an effective preconditioning technique for solving the nonsymmetric linear systems encountered in computation of incompressible flows in long domains. The application category we focus on is arterial fluid mechanics. These linear systems are solved using a nested iterative scheme with an outer Richardson scheme and an inner iteration that is handled via a Krylov subspace method. Test computations that demonstrate the robustness of our nested scheme are presented.

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Cited by 53 publications
(20 citation statements)
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“…A recent demonstration of this potential can be found in [53,57,58,64]. Segregated equation solver techniques recently developed by the T AFSM for FSI computations were described in Section 6 of [52].…”
Section: Segregated Equation Solversmentioning
confidence: 98%
See 1 more Smart Citation
“…A recent demonstration of this potential can be found in [53,57,58,64]. Segregated equation solver techniques recently developed by the T AFSM for FSI computations were described in Section 6 of [52].…”
Section: Segregated Equation Solversmentioning
confidence: 98%
“…Model-2 required 500 GMRES iterations for good mass balance, at least partly because there are significantly more elements along the flow direction. As pointed out in [31], this is a significant increase in computational cost, so we are exploring better preconditioners, such as the one in [53]. For all six nonlinear iterations, for Model-1 and Model-3 the fluid scale is 1.0 and the structure scale is 50.…”
Section: Computations With New Surface Extraction Mesh Generation Anmentioning
confidence: 99%
“…Transonic flow past a sphere was also reported in 2006 [52]. The FSI computations reported in 2007 [5,[53][54][55][56][57] and 2008 [58][59][60][61][62][63] were for flow past a flag, patient-specific models of a middle cerebral artery with aneurysm and a birfucating middle cerebral artery with aneurysm, carotid artery birfucation, abdominal aortic aneurysms, parachutes with complex designs, a cloth piece falling over a rigid rod, flow in a tube constrained with a diaphragm, inflation of a balloon, flow through and around a windsock, descent of a T-10 parachute with fabric porosity, sails, Orion spacecraft parachutes, flow around two flexible spheres colliding, and a flexible sphere sliding past a constriction in a channel.…”
Section: Years 2001-2010mentioning
confidence: 88%
“…Model-2 requires 500 GMRES iterations for good mass balance, at least partly because there are significantly more elements along the flow direction. This represents a considerable increase in computational cost, hence we are exploring the possibility of using a better preconditioner, such as the one reported in [38]. Figure 5 shows the streamlines for each model when the volumetric flow rate is maximum.…”
Section: Remarkmentioning
confidence: 99%