Fluid-Structure Interaction Modelling of a Soft Pneumatic Actuator
Abstract
:1. Introduction
2. Materials and Methods
2.1. Fluid-Structure Interaction
- Navier–Stokes equations for the laminar, incompressible fluid flow:
- Equations of solid mechanics given by Newton’s second law:
2.2. Hyperelastic Material Model
2.3. PneuNets Bending Actuator
2.4. Coupled 2D FSI Modelling and Simulation
2.5. Coupled 3D FSI Modelling and Simulation
3. Results and Discussion
3.1. Deformation and Comparison with FEM Model
3.2. Initial Time Step Condition
3.3. Middle and Last Time Step Condition
3.4. Average Velocity of Fluid Domain
4. Conclusions and Outlook
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Appendix A
- Required modules in COMSOL: COMSOL Multiphysics Module, Structural Mechanics/MEMS Module, Nonlinear Structural Materials Module, CFD Module, and CAD Import Module
- Space dimension: three-dimensional model
- Physics: fluid–solid interaction
- Study type: stationary (gravity) and time-dependent (air pressure)
- Fluid mechanics: Air is chosen as material. Incompressible and laminar flow are selected. Gravity is included. Walls are treated with no slip condition. Material properties like dynamic viscosity and density of air are considered using a built-in function in COMSOL.
- Solid mechanics:
- ○
- Elastomer: Elastosil is assigned to the top and bottom parts, which is created as user-defined material with a density of 1130 kg/m3. The Yeoh hyperelastic material model is assigned using the model parameters given in Section 2.2.
- ○
- Paper: Paper is assigned to the interface boundary, and linear elastic material behaviour is applied. Paper is created as user defined material with required material properties of density = 750 kg/m3, Poisson’s ratio = 0.2, and Young’s modulus = 6.5 GPa [54].
- ○
- Contacts: The sidewalls of the chambers (except the left sidewall of the first chamber and the right sidewall of the last chamber) are assigned as contact pairs for the deformed configuration. All the left sidewalls are considered as source and the right sidewalls as destination for contact modelling. For the thin paper layer, another contact pair is created for the initial configuration. Contacts are modelled using the penalty condition.
- Moving mesh: The fluid domain is selected as deforming domain under a moving mesh. The Navier–Stokes equations given in (1) and (2) are solved in the deforming domain using Yeoh smoothing with C2 = 10. The prescribed mesh displacement of zero in all directions is applied to the inlet and the wall boundaries of the air supply tube above the first chamber.
- Boundary conditions: An inlet air pressure of 0.5 bar is applied at the inlet boundary. The pressure is applied using the ramp function, gradually increasing the pressure from 0 bar to 0.5 bar from t = 0 s to t = 1 s. The side and top walls of the first chamber are fixed, hence there is no displacement in all directions.
- Gravity is taken into account for the solid domain, and it acts in negative y direction.
- Fluid–structure interaction: The fluid domain is selected as deforming domain under a moving mesh and the walls of the fluid chambers are automatically assigned as the interface for fluid and solid. The fully coupled solver is selected for simulating fluid and solid domains.
- Mesh: The physics-controlled mesh is selected. The fine mesh is created predominantly with tetrahedral elements. The mesh is generated specifically in each domain and FSI interface. The total number of mesh elements is 1,022,609, in which 598,947 elements represent the fluid domain and are calibrated for fluid mechanics and 311,810 elements represent the solid domains. The minimum element quality based on skewness is 0.06.
- Study: Two study steps are implemented. Study Step 1 denotes a stationary study, which solves the model for gravity. Regarding this, the parameter t is defined with value zero in global definition. Study Step 2 denotes the time-dependent study, in which the inlet pressure is applied in time steps. The time steps are given as 0, 0.01, and 1 s. The inlet pressure increases for each time step by 500 Pa.
- Solver: The segregated solver is selected for the time-dependent study. Compared to the fully coupled solver, the segregated solver approach requires less memory and computation time.
- Cluster specifications: The model is computed on 24 cores running at 2.5 GHz. It takes 18 h and 43 min to compute.
Appendix B
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Sylgard | Elastosil | Ecoflex | |
---|---|---|---|
Manufacturer | Dow Corning | Wacker Chemie | Smooth-On |
Type | 184 | M4601 | 00–30 |
Colour | transparent | reddish brown | translucent |
Shore hardness | 50 A | 28 A | 00–30 |
Tensile strength | 6.76 MPa | 6.50 MPa | 1.38 MPa |
Density | 1.04 g/cm3 | 1.13 g/cm3 | 1.07 g/cm3 |
Elongation at break | 150% | 700% | 900% |
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Maruthavanan, D.; Seibel, A.; Schlattmann, J. Fluid-Structure Interaction Modelling of a Soft Pneumatic Actuator. Actuators 2021, 10, 163. https://doi.org/10.3390/act10070163
Maruthavanan D, Seibel A, Schlattmann J. Fluid-Structure Interaction Modelling of a Soft Pneumatic Actuator. Actuators. 2021; 10(7):163. https://doi.org/10.3390/act10070163
Chicago/Turabian StyleMaruthavanan, Duraikannan, Arthur Seibel, and Josef Schlattmann. 2021. "Fluid-Structure Interaction Modelling of a Soft Pneumatic Actuator" Actuators 10, no. 7: 163. https://doi.org/10.3390/act10070163