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Demonstration of PIV in a Transonic CompressorParticle Imaging Velocimetry (PIV) is a powerful measurement technique which can be used as an alternative or complementary approach to Laser Doppler Velocimetry (LDV) in a wide range of research applications. PIV data are measured simultaneously at multiple points in space, which enables the investigation of the non-stationary spatial structures typically encountered in turbomachinery. Many of the same issues encountered in the application of LDV techniques to rotating machinery apply in the application of PIV. Preliminary results from the successful application of the standard 2-D PIV technique to a transonic axial compressor are presented. The lessons learned from the application of the 2-D PIV technique will serve as the basis for applying 3-component PIV techniques to turbomachinery.
Document ID
19980000417
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wernet, Mark P.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1997
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-113164
NAS 1.15:113164
E-10921
Report Number: NASA-TM-113164
Report Number: NAS 1.15:113164
Report Number: E-10921
Meeting Information
Meeting: Symposium on Nonintrusive Measurement Techniques for Propulsion Engines
Location: Brussels
Country: Belgium
Start Date: October 20, 1997
End Date: October 24, 1997
Sponsors: Advisory Group for Aerospace Research and Development
Funding Number(s)
PROJECT: RTOP 519-20-53-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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