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 ...

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 work, passive control of vortex shedding behind a circular cylinder by splitter plates of various lengths attached on the cylinder base is experimentally investigated in shallow ...