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The Design – Fluid-Structure Interaction (FSI) on Formula 1 Front Wing | ANSYS Fluent

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Fluid-Structure Interaction (FSI) interacts with some moving or deformable structures with or around an internal fluid flow. The interaction between fluid and structure is studied steadily and vibrationally. In the vibrational interaction, the strain formed in the solid structure forces the structure to move and shape, which is believed to be reducing the source of the strain, and the structure is reestablished in its original form (in fact the nature of the vibrational in the interaction between the structure and the fluid Is like a repetitive pattern).

The study of the effect of fluid on solid is one of the phenomena that has been highly regarded in recent years. This interaction can have many effects on the structure and can bring a lot of adverse results.

In this analysis, it has been tried to simulate and analyze the Fluid-Structure Interaction (FSI) on Formula 1 front wing as an FSI using Ansys Fluent software.

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The Design – Fluid-Structure Interaction (FSI) on Formula 1 Front Wing | ANSYS Fluent

Fluid-Structure Interaction (FSI) interacts with some moving or deformable structures with or around an internal fluid flow. The interaction between fluid and structure is studied steadily and vibrationally. In the vibrational interaction, the strain formed in the solid structure forces the structure to move and shape, which is believed to be reducing the source of the strain, and the structure is reestablished in its original form (in fact the nature of the vibrational in the interaction between the structure and the fluid Is like a repetitive pattern).

The study of the effect of fluid on solid is one of the phenomena that has been highly regarded in recent years. This interaction can have many effects on the structure and can bring a lot of adverse results.

In this analysis, it has been tried to simulate and analyze the Fluid-Structure Interaction (FSI) on Formula 1 front wing as an FSI using Ansys Fluent software.

Geometry & Grid

The geometry required for this analysis was generated by Ansys Design Modeler software. The meshing required for this analysis was also generated by Ansys Meshing software. The mesh type used in this analysis is unstructured. The total number of volume properties for geometry is 5,6037 m³.

Model

In this analysis, the k-epsilon (2 equation) turbulence viscosity model is used to check the fluid flow. The standard wall function is used near the wall.

Boundary Condition

The flow of primary air input design modeler geometry for this analysis is considered as velocity magnitude and is 3 m/s. The turbulence of the design modeler is set with an intensity equal to 5 %. The turbulence viscosity ratio of the design modeler is set with a viscosity ratio of 10.

The flow output range is also considered as a pressure outlet for the flow output region and gauge pressure is equal to 0. The inner wall is also considered a Stationary Wall.

Discretization of Equations

In this analysis, high-resolution is used for the advection scheme of the basic settings. In this analysis, the second-order is used for turbulence numerics. In this analysis, the residual type of convergence criteria is RMS and the residual target of convergence criteria is 1.E-6.

The results are presented as pressure contours as well as volume rendering.

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