47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2009
DOI: 10.2514/6.2009-924
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Supersonic Inlet Flow Control Using Plasma Actuators

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Cited by 36 publications
(21 citation statements)
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“…Webb et al 66 found that the impact on the SBLI region was simply to shift it upstream. This is a somewhat different conclusion to Caraballo et al 62 who suggested that actuation by LAFPA's increased the boundary layer velocity. Webb et al 66 and Caraballo et al 62 also disagree on the mechanism of control itself.…”
Section: Applications Of Lafpa'scontrasting
confidence: 53%
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“…Webb et al 66 found that the impact on the SBLI region was simply to shift it upstream. This is a somewhat different conclusion to Caraballo et al 62 who suggested that actuation by LAFPA's increased the boundary layer velocity. Webb et al 66 and Caraballo et al 62 also disagree on the mechanism of control itself.…”
Section: Applications Of Lafpa'scontrasting
confidence: 53%
“…This is a somewhat different conclusion to Caraballo et al 62 who suggested that actuation by LAFPA's increased the boundary layer velocity. Webb et al 66 and Caraballo et al 62 also disagree on the mechanism of control itself. Caraballo et al 62 suggested that the excitation of the SBLI unsteadiness was the main mechanism however Webb et al 66 suggested that simply the heating of the boundary layer is the control mechanism.…”
Section: Applications Of Lafpa'scontrasting
confidence: 53%
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