Abstract: Within the scope of this study, a quantitative investigation was carried out employing the particle image velocimetry (PIV) technique to determine vortical flow characteristics of 70°/40°, 70°/50°, and 70°/55° double delta ...

Abstract: 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 visualizations were carried out by particle ...

Abstract: 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 range of 0°≤β≤20° were investigated ...