Bahman Jahromi

[ 1 ] - Effect of Wing Sweep Angle on the Vortex Interaction of a Tail-Wing Configuration

The goal of this investigation is to study the effect of wing sweep angle on the horizontal wing-body- tail configurations in subsonic flow. For this purpose, a series of wind tunnel tests were conducted on a model having a moveable horizontal tail and a wing planform with different sweep angles. Tests were performed at different tail deflection angles. Static surface pressure distribution over...