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An investigation of a free jet at low Reynolds numbersA comparison of the measured and calculated flow field properties of a nozzle of unusual design which was used to produce an incompressible, low Reynolds number jet is presented. The nozzle is essentially a porous metal plate which covers the end of a pipe. Results are presented for nozzle Reynolds numbers from 50 to 1000 with velocities of 100 or 200 ft/sec. The nozzle produces a uniform velocity profile at nozzle Reynolds numbers well below those at which conventional contoured nozzles are completely filled with the boundary layer. A jet mixing analysis based on the boundary layer equations accurately predicted the flow field over the entire range of Reynolds numbers tested.
Document ID
19730021501
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Greene, G. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-69566
Report Number: NASA-TM-X-69566
Accession Number
73N30233
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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