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Gas-phase flowrate effect on disintegrating cryogenic liquid-jetsTwo phase liquid and gaseous nitrogen flow in a pneumatic two fluid atomizer was investigated. Characteristic dropsize for cryogenic sprays were measured with a scattered light scanning instrument developed at NASA-Lewis. Tests were conducted primarily in the aerodynamic stripping regime of liquid jet atomization. At a sampling distance of bar-x=1.3 cm, the Sauter mean, D(sub 32), and volume median, D(sub v.5), drop diameters were measured and correlated with nitrogen gas flowrate, W(sub n), to give the following expressions: D sub 32 to the -1=210W(sub n) to the -1.33 and D(sub v.5) to the -1=150 W(sub n to the -1.33, where reciprocal diameters and gas flowrate are in cm (-1) and g/sec, respectively. The exponent 1.33 for nitrogrn gas flowrate, W(sub n), is the same as that predicted by atomization theory for liquid-jet breakup in high velocity gasflow. When the spray was sampled at axial distances of bar-x=2.5 and 4.5 cm downstream of the atomizer, the exponent decreased to 1.2 and 0.9, respectively. This was attributed to the loss of small droplets due to their rapid vaporization.
Document ID
19900001961
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ingebo, Robert D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.15:102357
E-5071
NASA-TM-102357
Report Number: NAS 1.15:102357
Report Number: E-5071
Report Number: NASA-TM-102357
Meeting Information
Meeting: International Congress on Fluid Mechanics
Location: Cairo
Country: Egypt
Start Date: January 2, 1990
End Date: January 4, 1990
Accession Number
90N11277
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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