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International Journal of Bioprinting                        CFD analysis for multimaterial bioprinting conditions



            Table 1. Rheological parameters of alginate and gelatin   solution was achieved when these parameters reached a
            solutions [34,42]                                  state of convergence.
                        Content     n          k [Pa s ]          To further investigate the effect of nozzle geometries
                                                    n
             Alginate   0.5 w/v%    0.977      0.032           (cylindrical and conical) and process parameters on cell
                        1.0 w/v%    0.895      0.119           viability, the flow rate, velocity magnitude, and shear stresses
                        1.5 w/v%    0.840      0.346           at the outlet, as well the axial discharge of the dispensing
                                                               pressure along the printing head, were evaluated for the
             Gelatin    7.0 w/v%    0.795      0.240           converged solution. A variety of nozzle outlet diameters,
                                                               ranging from 0.25 to 2.00 mm, were examined at different
            Materials to be printed through pneumatic (compressed   inlet pressures (0.1–3.0 bar) for both nozzle types.
            air), mechanical (piston or screw), or solenoid (electrical   2.2. Mesh independence test
            pulses) driven printheads must exhibit shear-thinning   The 3D flow domain of the KSM-integrated printing
            properties, as this behavior allows to reduce shear stresses   heads was discretized, using the selective meshing feature
            during the printing process and to enhance cell viability.   of ANSYS Workbench meshing tool to create as many
                          −1
            The shear rate γ˙(s ) can be defined as follows:
                                                               structured (hexahedral) elements as possible, and fill the
                  du   P                                     remaining parts with tetrahedron elements. In this case,
                      r                            (V)     as the printing head consists of multiple bodies, we used
                  dr  2 L                                     the patch conforming method for the Y-shaped main body
            where r (m) is the radius of the pipe, L (m). According to   including the KSM, and the sweep method for sweepable
            Metzner et al. , the generalized Reynolds number for a   bodies, such as barrels, and the other cylindrical parts
                       [41]
            shear-thinning fluid is given by:                  (Figure 1). The mesh quality was refined near the mixing
                    u 2 n D n                                elements, and inflation layers were created for the pipe walls,
               Re          n                         (VI)     to capture the flow fields more precisely in those places. To
                          2
                   k  n6                                    obtain reliable numerical results, grid-independence tests
                   8    n                                  were conducted for all needle geometries with varying
                                                               outlet diameters. These preliminary test results enabled to
            where D is the pipe diameter (m).                  establish the best node layout and cell density, for numerical
               In  this  study,  non-crosslinked  alginate and  gelatin   accuracy and computational load. Thus, a mesh sensitivity
            solutions  were  selected  as  the  working  fluids.  The   study was performed to observe how the outlet velocity
            rheological data for both materials arepresented in Table 1.  magnitude deviates as the number of grids increased. The
                                                               discretization of the models used in CFD simulations for
               In the simulations, all solid boundaries were
            considered as stationary walls, where the “nonslip”   both nozzle types is shown in Figure 1.
            boundary condition was applied. Moreover, by adjusting   As shown in Figure 2, the calculated maximum velocity
            the dispensing pressure at the inlet boundaries, different   magnitude was stabilized by increasing the number of
            Reynolds numbers were obtained for the flow domain.   elements. Grid independence was achieved for the cylindrical
            The outlet boundary condition was set as atmospheric   and conical nozzle models, with 6 × 10  elements and
                                                                                                 5
            pressure in all simulations. The stationary solver was used   8 × 10 , respectively, beyond that no substantial changes were
                                                                    5
            to  resolve  the  model,  and calculations were  carried  out   observed. Based on these preliminary convergence test results,
            using pressure–velocity coupling (Coupled algorithm).   a mesh of 7.3 × 10  and 9.8 × 10  elements were chosen as the
                                                                             5
                                                                                       5
            To discretize the momentum and pressure formulation, a   optimal mesh density, as it provides high accuracy of results
            second-order upwind method was used, while the least-  with a shorter computational time required for convergence.
            squares cell-based method was used for the gradients.   The maximum skewness for all model meshes were lower than
            The relaxation parameters for pressure and momentum   0.85, with a minimum value of 2.3 × 10  and a minimum
                                                                                              −5
            were set as 0.5 and set to 1.0, for body forces and density,   element quality of 0.09, which according to the literature is a
            respectively. For all simulations, the relative residuals of   nice evidence of good mesh quality .
                                                                                          [43]
            the velocity and continuity components were less than
            10 , after approximately 1000 iterations, corresponding to   2.3. Mixing index
              −5
            a reasonably short calculation time (≤30 min) on an Intel   The distributive capacity of the Kenics mixer was also
            processor with four cores. Convergence analysis was also   investigated for different flow velocities. Distributive
            tested, by monitoring the area-weighted average values of   mixing,  also  known  as  simple  or  extensive  mixing,
            the shear stress and the velocity at the outlet. A stationary   represents the spatial distribution of the components


            Volume 9 Issue 6 (2023)                         14                        https://doi.org/10.36922/ijb.0219
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