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The Isolated Synthetic Jet in Crossflow: A Benchmark for Flow Control SimulationAn overview of the data acquisition, reduction, and uncertainty of experimental measurements made of the flowfield created by the interaction of an isolated synthetic jet and a turbulent boundary layer is presented. The experimental measurements were undertaken to serve as the second of three computational fluid dynamics validation databases for Active Flow Control. The validation databases were presented at the NASA Langley Research Center Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control in March, 2004. Detailed measurements were made to document the boundary conditions for the flow and also for the phase-averaged flowfield itself. Three component Laser-Doppler Velocimetry, 2-D Particle Image Velocimetry, and Stereo Particle Image Velocimetry were utilized to document the phase-averaged velocity field and the turbulent stresses.
Document ID
20080014259
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Schaeffler, Norman W.
(NASA Langley Research Center Hampton, VA, United States)
Jenkins, Luther N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Publication Information
Publication: AIAA Journal
Publisher: American Inst. of Aeronautics and Astronautics
Volume: 44
Issue: 12
Subject Category
Aerodynamics
Funding Number(s)
OTHER: 23-762-55-MC
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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