4.5 Article

Separation control in duct flows

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JOURNAL OF AIRCRAFT
卷 39, 期 4, 页码 616-620

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AMER INST AERONAUT ASTRONAUT
DOI: 10.2514/2.2973

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Active control of separation in a duct flow is achieved using an array of fluidic actuators based on synthetic-jet technology. A two-dimensional serpentine duct model is designed to produce controlled separated flow in two configurations, in which the flow is either completely separated or has a separation bubble. An array of synthetic-jet actuators is placed within the separated flow domain in the diffuser section downstream of the onset of separation. Actuation leads to complete flow attachment up to U-in = 75 m/s (M approximate to 0.2) and to partial reattachment up to U-in = 105 m/s (M approximate to 0.3).

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