45th AIAA Aerospace Sciences Meeting and Exhibit 2007
DOI: 10.2514/6.2007-322
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Active Flow Control of Sprays with Synthetic Jets

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Cited by 4 publications
(6 citation statements)
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“…9b), data at nine flow rate ratios were collected, a set of three air flow rates (5.5 l/min, 11 l/min, and 16.5 l/min) at three normalized distances between the water intake level and the face of the spray nozzle, L w /d s = 0, 144, and 288. Note that for a given air flow rate, as L w /d s increases Q a /Q w decreases, as the volumetric flow rate of water increases when the nozzle siphons from a higher location (see Pavlova et al, 2007Pavlova et al, , 2008. Fig.…”
Section: Active Control Of Spray Coolingmentioning
confidence: 95%
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“…9b), data at nine flow rate ratios were collected, a set of three air flow rates (5.5 l/min, 11 l/min, and 16.5 l/min) at three normalized distances between the water intake level and the face of the spray nozzle, L w /d s = 0, 144, and 288. Note that for a given air flow rate, as L w /d s increases Q a /Q w decreases, as the volumetric flow rate of water increases when the nozzle siphons from a higher location (see Pavlova et al, 2007Pavlova et al, , 2008. Fig.…”
Section: Active Control Of Spray Coolingmentioning
confidence: 95%
“…Shadowgraphy measurements were acquired at 45 locations in the spray, such that the effect of active flow control could be determined for the entire three-dimensional spray. In the present paper, only data along the centerline of the spray are presented for brevity [for more details about the Shadowgraphy technique, including a complete description of droplet sizing and velocity measurements, as well as for the full 3D field, see previous work by Pavlova et al (2007Pavlova et al ( , 2008]. In these measurements, the resulting uncertainty in the velocity is ±0.1 m/s and ±0.5 lm in the droplet diameter.…”
Section: Experimental Setup and Proceduresmentioning
confidence: 97%
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