The ground effect influences the flow structure on a delta wing during landing and take-off
processes. In this regard, comprehensive instantaneous velocity measurements and flow …

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 leading-edge sweep angle significantly influences the flight performance of swept
wings. The vortex flow structures affect the flow behavior of the moderate to highly swept …

The flow fields over a generic cranked double delta wing were investigated. Pressure and
velocity distributions were obtained using a Pitot tube and a hot wire anemometer. Two …

Lambda wing, as a commonly used configuration for modern combat aircraft, tend to reduce
stability margin known as Pitch-Break before the wing completely stalls. This phenomenon …

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 …

In the present investigation, flow structures over a slender delta wing with a 70° sweep
angle, Λ at an angle of attack, α of 30°, and under the variation of yaw angles within the …

The effects of thickness-to-chord (t/c) ratio, anhedral angle (δ), and cropping ratio from
trailing-edge (C r%) on the aerodynamics of non-slender reverse delta wings in comparison …

One of the factors significantly influencing the flow structures and vortices formed on delta
wings is the shape of the leading edge. This study examined the impact of needle vortex …

Flight condition of aircrafts proximity to the ground, so-called “Ground Effect”(GE), is among
one of the most recent research areas since the aerodynamic performance and stability of …