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Cryogenic spray vaporization in high-velocity helium, argon and nitrogen gasflowsEffects of gas properties on cryogenic liquid-jet atomization in high-velocity helium, nitrogen, and argon gas flows were investigated. Volume median diameter, D(sub v.5e), data were obtained with a scattered-light scanning instrument. By calculating the change in spray drop size, -Delta D(sub v.5)(exp 2), due to droplet vaporization, it was possible to calculate D(sub v.5C). D(sub v.5C) is the unvaporized characteristic drop size formed at the fuel-nozzle orifice. This drop size was normalized with respect to liquid-jet diameter, D(sub O). It was then correlated with several dimensionless groups to give an expression for the volume median diameter of cryogenic LN2 sprays. This expression correlates drop size D(sub v.5c) with aerodynamic and liquid-surface forces so that it can be readily determined in the design of multiphase-flow propellant injectors for rocket combustors.
Document ID
19940012973
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ingebo, Robert D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-106363
AIAA PAPER 94-0687
E-8161
NAS 1.15:106363
Report Number: NASA-TM-106363
Report Number: AIAA PAPER 94-0687
Report Number: E-8161
Report Number: NAS 1.15:106363
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N17446
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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