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Turbulence measurements in a swirling confined jet flowfield using a triple hot-wire probeAn axisymmetric swirling confined jet flowfield, similar to that encountered in gas turbine combustors was investigated using a triple hot-wire probe. The raw data from the three sensors were digitized using ADC's and stored on a Tektronix 4051 computer. The data were further reduced on the computer to obtain time-series for the three instantaneous velocity components in the flowfield. The time-mean velocities and the turbulence quantities were deduced. Qualification experiments were performed and where possible results compared with independent measurements. The major qualification experiments involved measurements performed in a non-swirling flow compared with conventional X-wire measurements. In the swirling flowfield, advantages of the triple wire technique over the previously used multi-position single hot-wire method are noted. The measurements obtained provide a data base with which the predictions of turbulence models in a recirculating swirling flowfield can be evaluated.
Document ID
19830006163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Janjua, S. I.
(Dynamics Technology, Inc. Torrance, CA, United States)
Mclaughlin, D. K.
(Dynamics Technology, Inc. Torrance, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 27, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:169668
DT-8178-02
NASA-CR-169668
Report Number: NAS 1.26:169668
Report Number: DT-8178-02
Report Number: NASA-CR-169668
Accession Number
83N14434
Funding Number(s)
CONTRACT_GRANT: NAG3-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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