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Control and Identification of Turbulent Boundary Layer SeparationEffective delay of turbulent boundary layer separation could be achieved via closed-loop control. Constructing such a system requires that sensor data be processed, real-time, and fed into the controller to determine the output. Current methods for detection of turbulent boundary layer separation are lacking the capability of localized, fast and reliable identification of the boundary layer state. A method is proposed for short-time FFT processing of time series, measured by hot-film sensors, with the purpose of identifying the alternation of the balance between small and large scales as the boundary layer separates, favoring the large scales. The method has been validated by comparison to other criteria of separation detection and over a range of baseline and controlled flow conditions on a simplified high-lift system, incorporating active flow control.
Document ID
20040111309
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Seifert, Avi
(Telasic Communications, Inc. El Segundo, CA, United States)
Pack-Melton, La Tunia
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Aerodynamics
Meeting Information
Meeting: International Union of Theoretical and Applied Mechanics 2004
Location: Gottingen
Country: Germany
Start Date: August 12, 2004
End Date: August 14, 2004
Sponsors: International Union of Theoretical and Applied Mechanics.
Funding Number(s)
OTHER: 23-719-55-MG
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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