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Measurement of Separated Flow Structures Using a Multiple-Camera DPIV SystemA novel multiple-camera system for the recording of digital particle image velocimetry (DPIV) images acquired in a two-dimensional separating/reattaching flow is described. The measurements were performed in the NASA Langley Subsonic Basic Research Tunnel as part of an overall series of experiments involving the simultaneous acquisition of dynamic surface pressures and off-body velocities. The DPIV system utilized two frequency-doubled Nd:YAG lasers to generate two coplanar, orthogonally polarized light sheets directed upstream along the horizontal centerline of the test model. A recording system containing two pairs of matched high resolution, 8-bit cameras was used to separate and capture images of illuminated tracer particles embedded in the flow field. Background image subtraction was used to reduce undesirable flare light emanating from the surface of the model, and custom pixel alignment algorithms were employed to provide accurate registration among the various cameras. Spatial cross correlation analysis with median filter validation was used to determine the instantaneous velocity structure in the separating/reattaching flow region illuminated by the laser light sheets. In operation the DPIV system exhibited a good ability to resolve large-scale separated flow structures with acceptable accuracy over the extended field of view of the cameras. The recording system design provided enhanced performance versus traditional DPIV systems by allowing a variety of standard and non-standard cameras to be easily incorporated into the system.
Document ID
20010098617
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Humphreys, William M., Jr.
(NASA Langley Research Center Hampton, VA United States)
Bartram, Scott M.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 10, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 19th International Congress on Instrumentation in Aerospace Simulation Facilities
Location: Cleveland, OH
Country: United States
Start Date: August 27, 2001
End Date: August 30, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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