Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications

An airfoil tip vortex mitigation device comprising an intake port disposed in a first surface of an airfoil and an exit port in fluid communication with the intake port and disposed in a second surface of the airfoil where air pressure is less than at the first surface when the airfoil is producing...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WOODEN PERRY, CHARLTON ERIC F, AZEVEDO JEFFREY J, BLOSCH EDWIN L, MILLER DANIEL N, MOOR RUBLE E
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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