Menu

Executive Programs

Workshops

Projects

Blogs

Careers

Student Reviews



More

Academic Training

Informative Articles

Find Jobs

We are Hiring!


All Courses

Choose a category

Loading...

All Courses

All Courses

logo

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.

  • Mechanical Engineering
  • Automotive Engineering
  • Materials Engineering
  • Aerospace Engineering
  • Aeronautical Engineering

duration
Duration :

1 month

projectfees
Project Fees :

INR 30,000

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.

What will you do in this project?

Step 1 - Geometry creation in Converge Studio

Step 2 - Creating a virtual wind tunnel in Converge Studio

Step 3 - Apply Boundary Conditions and Run the Simulation

Calculations and Analysis

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

Similar Projects you might be interested:

Flow over a Mercedes Benz Actros Truck using StarCCM+
This project deals with simulating the flow around a Mercedes Benz Actros truck with and without the trailer attachment, We will be studying the production of wake and how the trailer attachment affects the wake produced by the tractor and the effect this has on the production of drag on the vehicle. Suitable reports and plots will be used to measure the drag coefficient and to assess convergence. Various post processing techniques can be used to provide animations that clearly show the flow patterns.
duration
Duration:

1 month

domainname
Domain :

Mechanical Engineering , Automotive Engineering , Materials Engineering , Aerospace Engineering , Aeronautical Engineering

Know more
In this project, you will be setting up the cases for the FSAE racing car in Converge CFD software and then simulating them to analyse the drag force and the down force experienced by each component of the FSAE car.
duration
Duration:

1 month

domainname
Domain :

Mechanical Engineering , Automotive Engineering , Materials Engineering , Aerospace Engineering , Aeronautical Engineering

In this project, you will perform a transient flow over a circular cylinder and post-process the results in SolidWorks Flow Simulation to understand the effect of vortex shedding due to the change in the Reynolds number
duration
Duration:

1 month

domainname
Domain :

Mechanical Engineering , Automotive Engineering , Aerospace Engineering , Aeronautical Engineering

This project deals with simulating the flow around an Ahmed Body, which is a prototypical car model. In order to perform this simulation, a computational domain will be defined in the form of a virtual wind tunnel. The simulation will be run for 25 and 35° slant angles and the flow patterns will be studied for both cases. Multiple cases for various slant angles can be run to show how the separation at the rear takes place and how the wake is affected, ultimately affecting the drag produced by the body. Finally, the results will be compared with the experimental results to get an idea of which solution and turbulence models to use and fine tune the setup to provide the best results.
duration
Duration:

1 month

domainname
Domain :

Mechanical Engineering , Automotive Engineering , Materials Engineering , Aerospace Engineering , Aeronautical Engineering

In this project, you will be creating the geometry and setting up the case in Converge Studio. And then simulating to analyze the drag and the down force experienced by the Ahmed body. You will also be performing the validation study.
duration
Duration:

1 month

domainname
Domain :

Mechanical Engineering , Automotive Engineering , Materials Engineering , Aerospace Engineering , Aeronautical Engineering

Showing 1 of 5 projects

Project Highlights

The project is an advanced level project

Pre-requisites

Work with Multiple Tools

showcase

Flow over an Airfoil NACA 2412

In this project, you will be creating a geometry either in Converge Studio or any of the CAD package and setting up the case in Converge Studio by providing appropriate boundary conditions. Also, you will be learning the theory behind how to create a virtual wind tunnel and will be creating it. Through this project, you will be getting a very good insight on the concepts of Turbulence modelling, Y+, calculating 1st cell height near the wall and also understand how to make use of Y+ calculator to calculate base grid size. You will get exposed to very strong features of fixed embedding, volume refinement, boundary layer generation which are really important as it gives user, a very good control on the cell count and cell count can easily be optimized using these features. You will also be making few pen and paper calculation in order to calculate drag co-efficient and lift co-efficient for different angle of attacks. Also, you will be exporting the data into MS Excel to create meaningful plots.