| HTML |
|---|
<div style="background-color: yellow; border: 2px solid red; margin: 4px; padding: 2px; font-weight: bold; text-align: center;">
This page has been moved to <a href="https://courses.ansys.com/index.php/courses/flow-over-an-airfoil/">https://courses.ansys.com/index.php/courses/flow-over-an-airfoil/</a>
<br>
Click in the link above if you are not automatically redirected in 10 seconds.
</div>
<meta http-equiv="refresh" content="10; URL='https://courses.ansys.com/index.php/courses/flow-over-an-airfoil/'" /> |
| Include Page |
|---|
| Flow over an Airfoil - Panel |
|---|
| Flow over an |
|---|
|
...
...
...
Flow over an Airfoil
Created using ANSYS 14.0
Problem Specification
In this tutorial, we will show you how to simulate a NACA 0012 Airfoil at a 6 degree angle of attack placed in a wind tunnel. Using FLUENT, we will create a simulation of this experiment. Afterwards, we will compare values from the simulation and data collected from experiment.
Image Modified
Continue
Go to Step 1 - : Pre-Analysis & Start-Up
Go to all FLUENT Learning Modules
See and rate the complete Learning Module
Sign-up for free online course on ANSYS simulations!