Effects of Active and Passive Flow Control on Dynamic-Stall Vortex Formation

An experimental investigation into the effects of a synthetic jet actuator working in concert with fixed vortex generators on a ramping NACA 0015 wing is explored.

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Veröffentlicht in:Journal of aircraft 2004-03, Vol.41 (2), p.405-408
Hauptverfasser: Traub, Lance W, Miller, Adam, Rediniotis, Othon
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Sprache:eng
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container_title Journal of aircraft
container_volume 41
creator Traub, Lance W
Miller, Adam
Rediniotis, Othon
description An experimental investigation into the effects of a synthetic jet actuator working in concert with fixed vortex generators on a ramping NACA 0015 wing is explored.
doi_str_mv 10.2514/1.2591
format Article
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subjects Aerodynamics
Aircraft
Applied fluid mechanics
Exact sciences and technology
Experiments
Flow control
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Generators
Physics
Rotational flow and vorticity
Separated flows
title Effects of Active and Passive Flow Control on Dynamic-Stall Vortex Formation
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