The Aeroelasticity Research Group at Texas A&M University

         
     

Videos

F-16 Limit Cycle Oscillation Videos

Video Clip #1
Video Clip #2
Video Clip #3
Video Clip #4




Animations of Experimental Data from the Texas A&M Nonlinear Aeroelastic Testing Aparatus (NATA)

Video Clip #1
Video Clip #2
Video Clip #3
Video Clip #4
Video Clip #5




Limit Cycle Oscillation Simulations Using The Unsteady Vortex Lattice Method (Courtesy of Dr. Dean Mook)

Video Clip #1
Video Clip #2
Video Clip #3
Video Clip #4

 
     
       
     
       
     
       
     
       
     
       
     
       
 

 

Texas A&M University

 

Dwight Look College of Engineering