Animation

Evolution of disturbance vorticity for a free-stream convecting vortex with speed, c = 0.3 and strength, \Gamma = 0.1

Evolution of vorticity magnitude in the mid-span plane of a tank with dimensions 150 x 150 x 25 mm showing the sequence of events in a typical RTI.

Evolution of numerical Schlieren for a natural laminar airfoil having a thermal control placed at x/c = 0.45 showing the control of a typical unsteady shock in a transonic SBLI event