You are viewing an old version of this page. View the current version.

Compare with Current View Page History

« Previous Version 3 Next »

 

Problem Specification

The airplane body below is subjected to 600 mile per hour winds at 0 degrees to simulate it traveling mid flight. In an effort to study the flow over the wing-body junction, the velocity vectors and streamlines will be calculated.

 


Go to Step 1: Start-Up

Go to all (ANSYS or FLUENT) Learning Modules

  • No labels