AMGCL
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Software:40929
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Source code repository: https://github.com/ddemidov/amgcl
Related Items (18)
Locally conservative immersed finite element method for elliptic interface problems ⋮ Three dimensional modeling of liquid droplet spreading on solid surface: an enriched finite element/level-set approach ⋮ Physics constrained learning for data-driven inverse modeling from sparse observations ⋮ Locally conservative discontinuous bubble scheme for Darcy flow and its application to Hele-Shaw equation based on structured grids ⋮ Subdomain deflation combined with local AMG: a case study using AMGCL library ⋮ The open porous media flow reservoir simulator ⋮ The meshless finite point method for transient elastodynamic problems ⋮ Partial reuse AMG setup cost amortization strategy for the solution of non-steady state problems ⋮ Mathematical modeling and experimental study of erosion-deposition process in deformable porous media ⋮ Topology optimization of Stokes flow with traction boundary conditions using low-order finite elements ⋮ Learning viscoelasticity models from indirect data using deep neural networks ⋮ Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number ⋮ An enriched finite element/level-set method for simulating two-phase incompressible fluid flows with surface tension ⋮ A unified arbitrary Lagrangian-Eulerian model for fluid-structure interaction problems involving flows in flexible channels ⋮ Topology optimization for minimum temperature with mass flow and stiffness constraints ⋮ A numerical study of the additive Schwarz preconditioned exact Newton method (ASPEN) as a nonlinear preconditioner for immiscible and compositional porous media flow ⋮ Моделирование влияния сдвига ветра на снижение лобового сопротивления энергоэффективного высотного сооружения с использованием дросселирующего эффекта ⋮ Effect of compressibility on the trapped vortex in the gap between the coaxial disk and cylinder and the drag of their arrangement for axisymmetric sub-, trans-, and supersonic flow
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