The development and formation of the leading-edge vortices due to the change in the angle
of attack, α, and yaw angle, θ, for a unique cross-flow plane at a dimensionless distance of …

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 …

The aim of this study is to qualitatively and quantitatively investigate the flow characteristics
of a nonslender diamond wing with a sweep angle of Λ= 40° by using dye visualization and …

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 …

DELTA wings have evolved over the years and are primarily used on many fighter aircraft.
As these aircraft become more and more maneuverable, delta-wing vortex dynamics and the …

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 …

Present investigation focuses on unsteady flow structures in end-view planes at the trailing
edge of delta wing, X/C= 1.0, where consequences of vortex bursting and stall phenomena …

The objective of this work is to reveal the significance of a trailing-edge attachment on the
flow structure over a generic nonslender delta wing using the dye visualization technique on …

The aim of this study is to investigate the time-averaged flow structure around a nonslender
diamond and lambda wing using a laser based 3-dimessional Particle Image Velocimetry …