2007
DOI: 10.1007/s00348-007-0362-7
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Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control

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Cited by 428 publications
(320 citation statements)
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“…Figure 15 shows the di¨usion of the transferred momentum from the plasma to the boundary layer. This is comparable to what can be observed in quiescent air [6]. The ionic wind is higher for a consumed power P/L = 80 W/m.…”
Section: Mean Velocity Pro¦lessupporting
confidence: 86%
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“…Figure 15 shows the di¨usion of the transferred momentum from the plasma to the boundary layer. This is comparable to what can be observed in quiescent air [6]. The ionic wind is higher for a consumed power P/L = 80 W/m.…”
Section: Mean Velocity Pro¦lessupporting
confidence: 86%
“…As the DBD actuator induces a pulsed body force at the same frequency f p as the input signal [6], it may excite the corresponding T-S waves and trigger a promoted transition if f p is not well chosen [5]. For this reason, boundary layer mean velocity pro¦les have been computed from the experimental pressure distribution using an ONERA in-house boundary layer code (3C3D) and linear stability has then been applied.…”
Section: Baseline Flowmentioning
confidence: 99%
“…The majority of experimental [12][13][14]16 and numerical 10,18 investigations on the DBD forcing mechanisms discuss the sine waveform, albeit for different carrier frequencies and applied voltages. The temporal evolution of velocity and acceleration in the plasma region is presented in Fig.…”
Section: A Sine Waveformmentioning
confidence: 99%
“…Time-resolved laser Doppler anemometry (LDA) measurements were conducted in quiescent air 12 where the asymmetry between the two half cycles is evident. Large momentum transfer during the negative half cycle was recorded which corresponds with the recent modeling efforts.…”
Section: Introductionmentioning
confidence: 99%
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