Abstract
A parallel fully-coupled fluid-structure interaction (FSI) algorithm [1] has been applied to the deformation of red blood cells (RBCs) in capillaries where cell deformability have significant effects on blood rheology. In the present FSI algorithm, the fluid domain is discretized using the side-centered unstructured finite volume method [2] based on Arbitrary Lagrangian-Eulerian (ALE) formulation, meanwhile the solid domain is discretized with the classical Galerkin finite element formulation for the Saint Venant-Kirchhoff material in a Lagrangian frame. In addition, the compatible kinematic boundary condition boundary condition [1] is applied at interface between the solid and fluid domains in order to satisfy the global discrete geometric conservation law (DGCL). Three important physical parameters for the blood flow are simulated and analyzed (i) the effect of the hematocrit density, (ii) the effect of the red cell spacing, and (iii) the effect of capillary radius. The results show that the cell deformation decreases with increasing hematocrit density which is also shown to play a significant role for velocity field. The capillary diameter is found out to be particularly important for the flow pressure gradient as well as the deformation of red blood cells. The numerical calculations indicate a rather complex shape deformation in which the biconcave discoid shape changes to a parachute-like shape which is in accord with the earlier results in the literature.
Original language | English |
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Title of host publication | 47th AIAA Fluid Dynamics Conference, 2017 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624105005 |
DOIs | |
Publication status | Published - 2017 |
Event | 47th AIAA Fluid Dynamics Conference, 2017 - Denver, United States Duration: 5 Jun 2017 → 9 Jun 2017 |
Publication series
Name | 47th AIAA Fluid Dynamics Conference, 2017 |
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Conference
Conference | 47th AIAA Fluid Dynamics Conference, 2017 |
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Country/Territory | United States |
City | Denver |
Period | 5/06/17 → 9/06/17 |
Bibliographical note
Publisher Copyright:© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.