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- W2002016415 abstract "The development of a laser-based combustion diagnostics system and its application to the analysis of a highpressure rocket engine injector e owe eld are described. One dimensionally spatially resolved (linewise), multispecies, single-pulseimages are obtained with an imaging spectrograph/digital camera detection setup that images spontaneousvibrational Raman light scattering caused by a pulsed ultraviolet laser, used to enhanceRaman signal strength by the inverse fourth power of laser wavelength scaling forRaman scattering cross sections. These images provide temporally and spatially resolved qualitative information about the presence of gaseous major species (water vapor and molecular hydrogen, nitrogen, and oxygen ) during a hot-e re, high-pressure (6.04-MPa) test of a single-element liquid oxygen/gaseous hydrogen swirled injector operating at a high oxidizer/fuel mixture ratio (100)inatestarticlepressurizedbyanitrogencoe ow.Ramanimages,takenevery40ms,aregenerallyuncorrelated with respect to each other during the constant pressure, main-stageportion of the test, but occasionally temporally adjacent imagepairsarecorrelated, suggesting large-scalemotion in thee ow, possibly from transverse movements of the reactant jet within the diluent coe ow. Simultaneous measurements of major species show unburnt ignitor gas (hydrogen) during the startup transient and excess diluent (nitrogen) during the shutdown transient, along with signie cant variations in the oxygen/nitrogen ratio during the test. Stimulated Raman and ozone production problems are investigated." @default.
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- W2002016415 date "2001-01-01" @default.
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- W2002016415 title "Development of Ultraviolet Raman Diagnostics for Rocket Engine Injector Analysis" @default.
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- W2002016415 doi "https://doi.org/10.2514/2.5703" @default.
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