INVESTIGATION OF HYSTERESIS EFFECTS ON A WING-FLAP CONFIGURATION AT HIGH-LIFT USING PIV

Investigation of hysteresis effects on a wing-flap configuration at high-lift using PIV

 

  1. Investigation of hysteresis effects on a wing-flap configuration at high-lift using PIV”, J of Aircraft, Vol. 43 No. 4, 2006.

Last updated on : 31-08-2020 09:51:23pm