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Workbench 17

Manufactured by ANSYS
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ANSYS Workbench 17.0 is a comprehensive engineering simulation platform that provides a unified, extensible, and flexible environment for automated engineering analysis. It enables seamless parametric, integrated multiphysics, and multidisciplinary analysis.

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9 protocols using workbench 17

1

Finite Element Analysis of Mouse Ulna

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FE analysis was conducted using ANSYS workbench 17.1 (ANSYS, Canonsburg, PA, USA) for a mouse ulna sample. Using microCT images, the proximal ulna was segmented and meshed with MIMICS 16 (Materialise, Leuben, Belgium) using the procedure previously described (27 ). The proximal ulna was meshed into ~110,000 tetrahedral elements. A lateral load of 1 N was applied to the proximal end of the ulna (elbow loading). The deformations and stresses resulting from the applied loads were computed. In this analysis, we employed Young’s modulus of 8.9 GPa and Poisson’s ratio of 0.35 for bone (27 , 28 (link)), and 0.5 MPa and 0.45 for soft tissue considering material properties of the skin and muscle of rodents (29 –31 (link)). We employed three loading and boundary conditions in response to elbow loading with 1-N loads: lateral loads applied at two opposing locations; lateral loads applied at a single site on one side and three supporting sites on the other side; and lateral loads on a pair of soft disks that sandwiched the elbow.
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2

Finite Element Modeling of Prostate Compression

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The FEM software employed for simulation was ANSYS Workbench 17.1 and
the component was Static Structural. An Ogden third model was used to fit the
measured strain-stress data. The simulation setup was configured to be identical
to the compression test. The contacts between the FEM model and plates were
defined as frictional with a friction coefficient of 10, and 137,905 nodes were
generated for the model with a size of 45.14 mm × 41.70 mm ×
30.95 mm (L × W × H). In the mesh section, the element size of
the prostate model was set to be 3 mm, and the surface size of the contacting
areas with the top and bottom plates was set to be 1 mm. The top and bottom
plates were meshed by sweeping in the Z-axis with one division separately, and
the edges were divided into 20 segments each with a bias factor of 5. The
element types were determined via ANSYS Workbench.
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3

Ultrasonic Fatigue Testing of CFRP

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To conduct ultrasonic fatigue loading on CFRP specimens, suitable geometry needs to be designed such that the specimen oscillates in its first transversal bending eigenmode due to resonance at 20 kHz [14 (link)]. This was determined using Ansys workbench 17.1 software with a homogeneous orthotropic material model based on six elastic moduli and three Poisson’s ratios (see Table 1) and the mass density. Some of these elastic constants were determined using standard monotonic tests according to DIN EN ISO 527-4 and DIN EN ISO 14129. Other values were estimated using the micromechanics model developed at the University of Twente [32 ]. The modal analysis from the finite element software resulted in a specimen geometry of 34 × 15 × 4.1 mm3 (see Figure 1b). The span between the support units, which can be seen in Figure 1a, was 18.6 mm. The distance between the nodal displacement points which can be visualized in Figure 1a, where relative displacement is zero, was chosen as the span length between the support units to reduce frictional heating during resonance oscillations.
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4

Biomechanical Analysis of Pedicle Subtraction Osteotomy

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The PSO model was imported into Ansys Workbench 17.0. The degree of freedom of sacrum was constrained in all directions, and its X, Y, and Z directions were set to 0 as the boundary condition. Stress on internal fixation, osteotomy plane, and displacement of plane was measured under various workloads, including stand forward flexion and backward extension, left and right flexion, and rotation. A 424.7-N axial load was applied on the T1 vertebral body, and bending, extension, and rotation were achieved with additional 10-Nm moment of force (22 ) (Table 2).
Overall stress distribution and displacement were measured on each internal fixation model and osteotomy planes, and the mechanical distribution of PSO models was compared under different workloads using numerical comparison.
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5

Finite Element Analysis of Material Configurations

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All the material configurations of this study were analysed by FEM analysis; the simulation platform was Ansys Workbench 17.0. 3D linear static simulations were performed.
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6

FEM Analysis of Tapered Dental Implants

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NobelReplace Select Tapered implants with sizes 3.5 × 10 mm, 4.3 × 10 mm, 3.5 × 11.5 mm, and 4.3 × 11.5 mm, and posterior mandibular segment (five regions) were selected using cone beam computed tomography (CBCT) scan. Cortical bone, cancellous bone, and implants were modeled using Creo 2.0. Twenty model assemblies were analyzed under FEM using ANSYS Workbench 17.0. Mechanical properties are shown in Table 1, contact types between the models are given in Table 2, and the forces applied in the abutment are given in Table 3. The models were subjected to axial (load 1) 100 N, non-axial buccolingual (load 2) 50 N, and non-axial mesiodistal (load 3) 50 N. From these loads, von Mises stress and strain values were evaluated. For statistical analyses, the four implants were grouped as G1, G2, G3, and G4, respectively. analysis of variance was used as statistical test.
Figure 1 shows The material properties applied to the cortical bone model, cancellous bone model, and implant model Figure 2 shows the stress distribution pattern in cortical and cancellous bone. Figure 3 shows the strain formation in cortical and cancellous bone. Figure 4 shows the strain formation in implant.
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7

Tensile Testing of Composite Laminate

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In ANSYS Workbench 17.0, after the construction of the laminated composite specimen as explained in Section 2.2, the shell element from ACP (Pre) domain was imported into implicit static structural analysis. The updated geometry required mesh generation. Then, the discretization of geometry, whereby the grid dependency tests of mesh elements were conducted. The mesh dependency check is carried out varying the number of elements and the best mesh of quadrilateral elements of 1625 is selected with good quality of 0.20. It should be noted that the maximum skewness of cell quality with the value towards 0 is indicated as the excellent cell quality with ideal and skewed quadrilaterals cell.
For boundary conditions of the tensile specimen, the first boundary condition of fixed support was assigned at the end grip with a tab of the rectangular specimen. While the second boundary condition was set to be towards the Z-axis with a force of 0 N. The other end of the rectangular specimen was assigned as the loading condition of load moving outward with a velocity of 20 mm/s until the specimen failed. The simulation ran for 10 s, with a time step of 0.1 s. The calculation was considered to be accomplished once the specimen failed. The simulation setup replicating the actual experiment for the tensile test is depicted in Figure 4.
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8

Biomechanical Comparison of Intact Ankylosing Spondylitis and Normal Vertebra

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In order to compare the range of motion (ROM) of intact AS model with the ROM of normal vertebra in biomechanical experiment, a 7.5 Nm moment and a compression 150N force [22 (link), 23 (link)] were applied at the center of the superior surface of T9. The inferior surface of L5 was immobilized. The ROM of T9-L5 was calculated and the ROM of the corresponding segment was compared with the previous experiment studies (Table 2). For testing the fixation capacity, a compressive load of 400 N force and a 10 Nm moment were applied in all fixation patterns [23 (link)–25 (link)]. Six loading conditions including flexion, extension, left bending, right bending, left axial rotation, and right rotation were simulated. Ansys workbench 17 (ANSYS Inc., PA, USA) was used to set the material properties and simulate the loading conditions.
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9

Computational Modeling of 3D Microfluidic Stenosis

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3D microfluidic model was constructed using Solidworks 2015 (Dassault Systèmes SolidWorks Corp.) and imported to ANSYS Workbench 17 (ANSYS, Inc.) for geometry discretization and numerical simulation using ANSYS FLUENT. Inlet flow velocity was set at 10 μl/min, which corresponded to ∼1 dyn/cm2. Non-slip boundary conditions were applied to all channel walls, and outlet was defined as a pressure outlet with atmospheric pressure. The Navier-Stokes equations were solved using 2nd order accuracy. The Semi-Implicit Method for Pressure-Linked Equations (SIMPLE) scheme was used for pressure-velocity decoupling. All simulations were conducted by using an iterative and segregated solution method. A residual sum for continuity and momentum of 1 × 10−6 was set as a convergence criterion. The working fluid was assumed to be water (homogeneous, single phase, Newtonian fluid, ρ =  993.37 kg/m3, μ  =  0.000692 kg/m s). To reduce computational load, only half of the chip was modelled due to channel symmetry along the midline. Mesh independence study was conducted. The optimized meshes for the 3D stenosis chip with 0%, 50%, and 80% of constrictions consisted of 2160, 86 678, and 137 892 cells, respectively.
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