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Area of Science:

  • Computational fluid dynamics
  • Biomedical engineering
  • Numerical analysis

Background:

  • Physiologically relevant pulmonary models are crucial for understanding lung mechanics.
  • Simulating these models efficiently on high-performance computing platforms is challenging.
  • Existing fluid-structure interaction (FSI) preconditioners are inadequate for lung models with algebraic constraints.

Purpose of the Study:

  • To develop efficient preconditioners for simulating complex pulmonary models.
  • To enable the assessment of mechanical ventilation strategies.
  • To contribute to designing patient-specific ventilation treatments.

Main Methods:

  • The study addresses a monolithic system from FSI with additional algebraic constraints, forming a saddle point problem.
  • The semi-implicit method for pressure-linked equations (SIMPLE) is employed to transform the saddle point problem into a standard FSI problem.
  • The proposed preconditioners are evaluated numerically on complex, patient-specific lung geometries.

Main Results:

  • The developed preconditioners demonstrate performance comparable to optimal multigrid methods.
  • The method effectively handles the multiphysics nature of the lung model.
  • The preconditioners are robust for physiologically relevant simulations with complex geometries.

Conclusions:

  • Efficient preconditioners have been developed for complex pulmonary models.
  • The SIMPLE-based approach successfully overcomes limitations of standard FSI preconditioners.
  • This methodology is applicable to other biomedical applications involving coupled flow and tissue deformation.