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 |
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container_end_page | 408 |
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container_issue | 2 |
container_start_page | 405 |
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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ispartof | Journal of aircraft, 2004-03, Vol.41 (2), p.405-408 |
issn | 0021-8669 1533-3868 |
language | eng |
recordid | cdi_proquest_miscellaneous_28184366 |
source | Alma/SFX Local Collection |
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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