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Sweeping Jet Actuator in a Quiescent EnvironmentThis study presents a detailed analysis of a sweeping jet (fluidic oscillator) actuator. The sweeping jet actuator promises to be a viable flow control actuator candidate due to its simple, no moving part structure and its high momentum, spatially oscillating flow output. Hot-wire anemometer and particle image velocimetry measurements were carried out with an emphasis on understanding the actuator flow field in a quiescent environment. The time averaged, fluctuating, and instantaneous velocity measurements are provided. A modified actuator concept that incorporates high-speed solenoid valves to control the frequency of oscillation enabled phase averaged measurements of the oscillating jet. These measurements reveal that in a given oscillation cycle, the oscillating jet spends more time on each of the Coanda surfaces. In addition, the modified actuator generates four different types of flow fields, namely: a non oscillating downward jet, a non oscillating upward jet, a non oscillating straight jet, and an oscillating jet. The switching from an upward jet to a downward jet is accomplished by providing a single pulse from the solenoid valve. Once the flow is switched, the flow stays there until another pulse is received. The oscillating jet is compared with a non oscillating straight jet, which is a typical planar turbulent jet. The results indicate that the oscillating jet has a higher (5 times) spreading rate, more flow entrainment, and higher velocity fluctuations (equal to the mean velocity).
Document ID
20140000479
Acquisition Source
Langley Research Center
Document Type
Conference Paper
External Source(s)
Authors
Koklu, Mehti
(NASA Langley Research Center Hampton, VA, United States)
Melton, Latunia P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 30, 2014
Publication Date
June 24, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-15692
Report Number: NF1676L-15692
Meeting Information
Meeting: AIAA Fluid Dynamics Conference and Exhibit
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 473452.02.07.03.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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