An airfoil active bleed system and related method. A housing includes an induction wall (39), an exhaust wall (40a,b) having one or more exhaust ports (44), and a chamber (41) between the induction and exhaust walls. Zero-net-mass-flux actuators (48) are located in the chamber and configured and positioned to collectively induct fluid through the induction wall (39) and selectively exhaust fluid through the exhaust port(s) (44).
Active bleed for airfoils
Aktives Ablassen für Luftschaufeln
Purge active pour surfaces portantes
25.04.2018
Patent
Elektronische Ressource
Englisch
Numerical Study of Ram Air Airfoils and Upper Surface Bleed-Air Control (AIAA 2014-2832)
British Library Conference Proceedings | 2014
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