Cryogenic spray vaporization in high-velocity helium, argon and nitrogen gasflows
Author(s) -
R. D. Ingebo
Publication year - 1994
Publication title -
32nd aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1994-687
Subject(s) - body orifice , vaporization , dimensionless quantity , propellant , helium , argon , drop (telecommunication) , nozzle , liquid nitrogen , volume (thermodynamics) , materials science , analytical chemistry (journal) , spray characteristics , chemistry , mechanics , jet (fluid) , thermodynamics , spray nozzle , physics , chromatography , ecology , organic chemistry , biology , telecommunications , computer science
Effects 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.
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