| 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/supersonic-flow-over-a-wedge-using-ansys-workbench/">https://courses.ansys.com/index.php/courses/supersonic-flow-over-a-wedge-using-ansys-workbench/</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/supersonic-flow-over-a-wedge-using-ansys-workbench/'" />
|
...
...
| Supersonic Flow Over a Wedge - Panel |
|---|
|
...
| Supersonic Flow Over a Wedge - Panel |
|---|
|
Supersonic Flow Over a Wedge
Created using ANSYS 13.0
| Note |
|---|
This tutorial has videos. If you are in a computer lab, make sure to have head phones. |
Problem Specification
A uniform supersonic stream encounters a wedge with a half-angle of 15 degrees as shown in the figure below.
...
Using FLUENT, calculate the Mach Number, static and total pressure behind the oblique shock that will be formed. Also, calculate the shock angle, pressure coefficient along the wedge and drag coefficient. Compare the FLUENT results with the corresponding analytical results.
Go to Step 1: Pre-Analysis & Start-Up
Go to all FLUENT Learning Modules
Sign-up for free online course on ANSYS simulations!