Magnetic Force Effect on an Airfoil CFD Simulation, ANSYS Fluent Tutorial
$270.00 Student Discount
- The problem numerically simulates Magnetic Force Effect on NACA 0015 airfoil using ANSYS Fluent software.
- We design the 3-D model by the Design Modeler software.
- We Mesh the model by ANSYS Meshing software.
- We use the MHD model to consider the magnetic force effect on the flow.
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Description
Description
The current project simulates Magnetic Force Effect on NACA 0015 airfoil using ANSYS Fluent software. We perform this CFD project and investigate it by CFD analysis.
This airfoil is a symmetrical airfoil that does not produce a lift force at zero attack angle. We investigate the lift coefficient of this airfoil at different attack angles with and without Magnetic Hydro-Dynamic (MHD).
In this problem, we study the separation and the maximum angle of attack where the separation does not occur. By applying the magnetic force (MHD), the separation happens at a larger angle of attack.
We have designed the present 2-D geometry by Design Modeler software. Also, an unstructured triangular mesh has been applied around the airfoil using ANSYS Meshing software.
Magnetic Force Methodology
In this project, we aim to investigate the magnetic field effect in the computational zone. We have enabled the MHD module in fluent software to consider the magnetic force effect on the flow.
Magnetic Force Conclusion
This project provides velocity and pressure counters, streamlines, and velocity vectors after applying the plasma actuator. As can be seen from the velocity contour, the plasma actuator’s application causes the flow in the boundary layer to accelerate and adhere to the surface of the airfoil.
Also, the leading edge pressure suction has increased, and as a result, the lift has increased. As it turns out, after applying the plasma actuator, the flow separates from the airfoil surface somewhere before the initial separation point, which means the separation is delayed.
Therefore, it can be concluded that by applying a plasma actuator (MHD) to the NACA 0015 airfoil; a static stall occurs at a larger angle of attack.
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Dell Marvin –
It was explained very wholly and accurately, and the expression and mastery of the MR-CFD are good and well and can be practical.
Josefina Corwin –
The topics and steps they used fully explained what would happen if you did or did not do it.
Ona Kautzer –
Your simulations are a great learning tool. They’ve really helped me understand complex phenomena.
MR CFD Support –
We’re delighted to hear that! Our goal is to make complex phenomena more understandable through our simulations. If you have any questions, don’t hesitate to ask
Mr. Robbie Goldner –
You have taught a very useful, useful and correct MR-CFD
Adonis Brown –
Could you explain more about how the mesh was generated in this simulation?
MR CFD Support –
Sure! We use ANSYS Meshing software to generate a high-quality mesh. The mesh was refined in areas of interest to accurately capture the effects of the magnetic force on the airfoil.
Haven Jakubowski –
I have a specific simulation that I’d like to see. Can I request that?
MR CFD Support –
Definitely! We’re always open to new ideas and would be happy to accommodate your request. Please provide more details about the simulation you’re interested in
Madilyn Hamill –
Do I get the UDF for MHD operations by purchasing this product?
MR CFD Support –
Yes, we will send you the relevant UDF.
Isabelle Cremin DDS –
I’m really impressed with the range of simulations you offer. There’s something for everyone!
MR CFD Support –
Thank you for your feedback! We strive to cover a wide range of topics and applications to cater to the diverse needs of our users.
Alexandra Murazik –
I noticed you use Design Modeler and SpaceClaim for modeling. Do you have any tips for someone new to these tools?
MR CFD Support –
Absolutely! Both tools are quite user-friendly. We recommend starting with the tutorials provided by ANSYS to get a good grasp of the basic functions. Don’t hesitate to reach out if you have specific questions.