CFD analysis of ONERA M6 wing using Fluent and validation with AGARD experimental data and high quality CFD from NASA
Sub Category
- Engineering
{inAds}
Objectives
- To conduct CFD analysis of ONERA M6 wing in particular and CFD analysis of any wing or aerodynamic body in general
- How to get high quality data from literature for validation
- Understanding drag, lift and pitching moment coefficient and reference values
- Setting up problem in Fluent and accelerating convergence
- Effect of turbulence model and Y+ values on aerodynamic coefficient
- Validating present CFD with avaiable experimental data and high quality CFD from NASA
- Effect of different solvers on results
Pre Requisites
- Basic understanding of aerodynamics and CFD
- Should be able to use Fluent on basic level
- Computer with i3 or better processor and 8 GB RAM. 16 GB RAM is recommended
- ANSYS 2022 R1 installed on your computer
FAQ
- Q. How long do I have access to the course materials?
- A. You can view and review the lecture materials indefinitely, like an on-demand channel.
- Q. Can I take my courses with me wherever I go?
- A. Definitely! If you have an internet connection, courses on Udemy are available on any device at any time. If you don't have an internet connection, some instructors also let their students download course lectures. That's up to the instructor though, so make sure you get on their good side!
{inAds}
Coupon Code(s)