Guided industry project
Flow over an Airfoil NACA 2412
In this project, you will be creating the geometry and setting up the cases for different angle of attacks in Converge Studio. And then simulating to analyze the drag and lift force experienced by an Airfoil at different angle of attacks.
- Duration
- 1 month
- Fee
- ₹30,000
- For
- B.E Mech/Aero/Auto/Production
What will you do in this project?
In this project, you will work on a NACA 2412 Airfoil and running cases for different angle of attacks (AOA). You will do the following in this project,
- Creating a geometry and the virtual wind tunnel
- Calculate the 1st cell height near the wall using Y+ calculator
- Setup and run the cases using Converge CFD software
- Line plotting and visualizing the results in PARAVIEW.
- Analyzing drag and lift force acting an an Airfoil at different AOA
Benefits of this Project
In this project, you will be creating the geometry and setting up the cases for different angle of attacks in Converge Studio. And then simulating to analyze the drag and lift force experienced by an Airfoil at different angle of attacks.The project is an advanced level project
- This project is great for undergraduate students (3rd & 4th year), M.Tech or MS students.
- If you are a working professional, this project will be helpful to learn CFD for Aerodynamics applications.
Pre-requisites
- Must be comfortable with CONVERGE
- Need basic background in CFD and Aerodynamics
- Need a basic knowledge on how to use command line window.
Work with Multiple Tools
- Work on Converge CFD software to setup the case.
- Use command line window (CYGWIN) to run simulations.
- Post process the results using PARAVIEW.
- Use of MS - WORD or GOOGLE DOC to create a report.
- Use MS - EXCEL to create meaningful plots,
Mechanical EngineeringAutomotive EngineeringMaterials EngineeringAerospace EngineeringAeronautical Engineering
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