Turbulent flow drag reduction

The present invention relates to apparatus for influencing fluid flow over a surface, and more particularly, but not exclusively, to turbulent boundary layer flow drag reduction for an aircraft. The present invention provides such apparatus including a plasma generator comprising first and second sp...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Scott, Simon J, Johnson, Graham A, Thornton, Edward
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The present invention relates to apparatus for influencing fluid flow over a surface, and more particularly, but not exclusively, to turbulent boundary layer flow drag reduction for an aircraft. The present invention provides such apparatus including a plasma generator comprising first and second spaced-apart independently controllable electrodes operable to cause a change in direction of the flow of the fluid over the surface.