The aerodynamic performance and the structure of vortical flow on a delta wing are affected
by the influence of the ground in take-off and landing stages. In this context, the effect of the …

The flow structure over a 35 deg swept delta wing is characterized in a low-speed wind
tunnel using techniques of laser-illuminated smoke visualization, laser Doppler …

In this paper, the effect of ground on aerodynamics and longitudinal static stability of a non-
slender delta wing with sweep angle of 45 degree and thickness-to-chord ratio (t/c) of 5.9 …

The ground effect (GE) on the formation of the vortical flow over a double delta wing having
sweep angles of Λ= 70°/40° was examined using the Particle Image Velocimetry (PIV) and …

The effect of unsteady blowing through the leading edge on the flow structure over a 45 deg
swept delta wing in relation to the steady blowing is experimentally studied in a low-speed …

The aim of the current study at first stage is to demonstrate the general flow structure
qualitatively using the dye visualization technique. Secondly, the instantaneous flow data …

In this study, extensive instantaneous velocity measurements were conducted within a flow
area by stereo particle image velocimetry (SPIV) to investigate the influence of the yaw …

The effect of passive bleeding on flow structure of a 45 deg swept delta wing is studied in a
low-speed wind tunnel using techniques of laser-illuminated smoke visualization, surface …

It is well known that the flow field over a delta wing is dominated by a pair of counter rotating
leading edge vortices (LEV). However, their mechanism is not well understood. The flow …

IN LINE with the progress achieved in unmanned aerial vehicle (UAVs), unmanned combat
aerial vehicle (UCAVs), and micro aerial vehicle (MAVs) technologies in recent decades …