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Stereo viewing 3-component, planar PIV utilizing fuzzy inferenceAn all electronic 3-D Digital Particle Image Velocimetry (DPIV) system has been developed for use in high velocity (supersonic) flows. Two high resolution CCD cameras mounted in a stereo viewing configuration are used to determine the out-of-plane velocity component from the difference of the in-plane velocity measurements. Double exposure image frames are acquired and Fuzzy inference techniques are used to maximize the validity of the velocity estimates obtained from the auto-correlation analysis. The CCD cameras are tilted relative to their respective lens axes to satisfy Scheimpflug's condition. Tilting the camera film plane ensures that the entire image plane is in focus. Perspective distortion still results, but can be corrected by proper calibration of the optical system. A calibration fixture is used to determine the experimental setup parameters and to assess the accuracy to which the z-plane displacements can be estimated. The details of the calibration fixture and procedure are discussed in the text. A pair of pulsed Nd:YAG lasers operating at 532 nm are used to illuminate the seeded flow from a convergent nozzle operated in an underexpanded condition. The light sheet was oriented perpendicular to the nozzle flow, yielding planar cross-sections of the 3-component velocity field at several axial stations. The key features of the supersonic jet are readily observed in the cross-plane vector plots.
Document ID
19960028020
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wernet, Mark P.
(NASA Lewis Research Center Cleveland,OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Instrumentation And Photography
Report/Patent Number
E-10278
NAS 1.15:107235
AIAA Paper 96-2268
NASA-TM-107235
Report Number: E-10278
Report Number: NAS 1.15:107235
Report Number: AIAA Paper 96-2268
Report Number: NASA-TM-107235
Meeting Information
Meeting: Advanced Measurement and Ground Testing Technology Conference
Location: New Orleans, LA
Country: United States
Start Date: June 17, 1996
End Date: June 20, 1996
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
96N29124
Funding Number(s)
PROJECT: RTOP 505-63-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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