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 : 13-10-2017 06:15:26pm