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Variable Frequency Diverter Actuation for Flow ControlThe design and development of an actively controlled fluidic actuator for flow control applications is explored. The basic device, with one input and two output channels, takes advantage of the Coanda effect to force a fluid jet to adhere to one of two axi-symmetric surfaces. The resultant flow is bi-stable, producing a constant flow from one output channel, until a disturbance force applied at the control point causes the flow to switch to the alternate output channel. By properly applying active control the output flows can be manipulated to provide a high degree of modulation over a wide and variable range of frequency and duty cycle. In this study the momentary operative force is applied by small, high speed isolation valves of which several different types are examined. The active fluidic diverter actuator is shown to work in several configurations including that in which the operator valves are referenced to atmosphere as well as to a source common with the power stream.
Document ID
20060047721
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Culley, Dennis E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-15675
NASA/TM-2006-214396
AIAA Paper 2006-3034
Report Number: E-15675
Report Number: NASA/TM-2006-214396
Report Number: AIAA Paper 2006-3034
Meeting Information
Meeting: 3rd Flow Control Conference
Location: San Francisco, CA
Country: United States
Start Date: June 5, 2006
End Date: June 8, 2006
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 581-02-08-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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