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Maximum two-phase flow rates of subcooled nitrogen through a sharp-edged orificeData are presented of an experiment in which subcooled liquid nitrogen was discharged through a sharp-edged orifice at flow rates near the maximum. The data covered a range of inlet stagnation pressures from slightly above saturation to twice the thermodynamic critical pressure. The data were taken along five separate inlet stagnation isotherms ranging from 0.75 to 1.035 times the thermodynamic critical temperature. The results indicate that subcooled liquids do not choke or approach maximum flow in an asymptotic manner even though the back pressure is well below saturation; and orifice flow coefficients are not constant as is frequently assumed. A metastable jet appears to exist which breaks down if the difference between back pressure and saturation pressure is large enough.
Document ID
19750018242
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simoneau, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-X-71760
Report Number: NASA-TM-X-71760
Meeting Information
Meeting: Cryog. Eng. Conf.
Location: Kingston, Ontario
Country: Canada
Start Date: July 22, 1975
End Date: July 25, 1975
Accession Number
75N26314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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