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The velocity and vorticity fields of the turbulent near wake of a circular cylinderThe purpose of this research is to provide a detailed experimental database of velocity and vorticity statistics in the very near wake (x/d less than 10) of a circular cylinder at Reynolds number of 3900. This study has determined that estimations of the streamwise velocity component in flow fields with large nonzero cross-stream components are not accurate. Similarly, X-wire measurements of the u and v velocity components in flows containing large w are also subject to the errors due to binormal cooling. Using the look-up table (LUT) technique, and by calibrating the X-wire probe used here to include the range of expected angles of attack (+/- 40 deg), accurate X-wire measurements of instantaneous u and v velocity components in the very near wake region of a circular cylinder has been accomplished. The approximate two-dimensionality of the present flow field was verified with four-wire probe measurements, and to some extent the spanwise correlation measurements with the multisensor rake. Hence, binormal cooling errors in the present X-wire measurements are small.
Document ID
19950015537
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wallace, James
(Maryland Univ. College Park, MD., United States)
Ong, Lawrence
(Maryland Univ. College Park, MD., United States)
Moin, Parviz
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:110513
NASA-TM-110513
Report Number: NAS 1.15:110513
Report Number: NASA-TM-110513
Accession Number
95N21954
Funding Number(s)
CONTRACT_GRANT: NCC2-5003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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