2016
DOI: 10.1134/s0869864316050024
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Flow control of the semicircular airfoil with a vortex cell at slot suction of air and its blowout into the near wake

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Cited by 9 publications
(3 citation statements)
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“…Placement of a vortex cell on the surface of a semicircular airfoil with slit suction and ejection into the near wake leads to the reconstruction of the unsteady separation pattern of low-velocity flow around the airfoil [15]. In this case, the flow separation point shifts to the trailing edge of the airfoil, the lift from ultra-low negative becomes positive, and the drag is halved.…”
Section: Of 16mentioning
confidence: 99%
“…Placement of a vortex cell on the surface of a semicircular airfoil with slit suction and ejection into the near wake leads to the reconstruction of the unsteady separation pattern of low-velocity flow around the airfoil [15]. In this case, the flow separation point shifts to the trailing edge of the airfoil, the lift from ultra-low negative becomes positive, and the drag is halved.…”
Section: Of 16mentioning
confidence: 99%
“…Placing a vortex cell on a semicircular airfoil's surface, accompanied by slit suction and ejection into the nearby wake, results in reconstructing the low-velocity flow's unsteady separation pattern around the airfoil [20]. The separation point of the flow shifts to the airfoil's trailing edge, and the lift changes from ultra-low negative to positive, while the drag is decreased by half.…”
Section: Introductionmentioning
confidence: 99%
“…This is of key interest, for instance, for efficient ventilation and cooling in gas turbines [4], microelectronics, and other industries, as well as to design actuators actively affecting the flow (see e.g. [5,6]) to reduce the skin friction, the aircraft drag, to increase the lift force and, therefore, to save fuel.…”
Section: Introductionmentioning
confidence: 99%