top of page

Xfoil Airfoil Simulation 

     For an aerospace lab, one part required simulating an airfoil inside XFoil. I was responsible for completing this part of the lab. The airfoil data can be found here. I loaded this data into xfoil, and increased the panel number to 300 for more accurate results (shown below). 

 

 

     The flow settings were changed to correspond to the experiment conducted in laboratry, and the following graphs were generated for angles of attack ranging from -15 degrees to 15 degrees. Xfoil approximated pressure and drag data using convergence techniques. 

 

 

 

 

bottom of page