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The Design – CFD Analysis of a 2D Simple Airfoil NACA-0009 Steady State Subsonic Flow | ANSYS Fluent

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Today’s, airfoils are used in a variety of industries that can be referred to as air industries. One of the ways to improve airfoil performance is to create forces such as magnetic force.

In this analysis simulation of flow through the NACA-0009 airfoil with magnetic force has been studied.

The Design – CFD Analysis of a 2D Simple Airfoil NACA-0009 Steady State Subsonic Flow | ANSYS Fluent

Today’s, airfoils are used in a variety of industries that can be referred to as air industries. One of the ways to improve airfoil performance is to create forces such as magnetic force.

In this analysis simulation of flow through the NACA-0009 airfoil with magnetic force has been studied.

Geometry & Grid

Geometry and mesh have been generated in Design Modeler and Ansys meshing software respectively. Cell types are unstructured.

Model

In this analysis, k-epsilon Realizable model has been used to simulate the flow turbulency flow. In this analysis, a pressure-based solver is used.

Boundary Condition

The inlet has been defined as Velocity Inlet. Wall boundary condition is also used for up and down of the airfoil.

Discretization of Equations

To solve the equations, the COUPLED algorithm is used in the second-order model.

Finally, results are represented as velocity and pressure contours.

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