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Shear coaxial injector instability mechanismsAlthough stable operating regimes for cryogenic coaxial injectors have been empirically determined, there is no knowledge of the spray characteristics corresponding to stable operation, or the physical processes which produce the atomization patterns that result in stable or unstable operation. The current engineering method for determining the stable operating regime of a cryogenic coaxial injector is the 'hydrogen temperature ramping' method, however there is no definitive knowledge of whether the hydrogen temperature influences the chamber stability by decreasing the injected gas velocity, by affecting a recirculation region at the base of the LOX Post, or by changing the pressure drop across the injector, allowing chamber pressure oscillations to couple to the fuel feed system. Results for the injector response from a linearized lumped-element model are presented as a function of temperature and frequency. LDV measurements in the recess region at the base of the LOX post show reverse flow indicative of a recirculation region. Finally, Phase Doppler Particle Analyzer (PDPA) measurements of droplet size and velocity distributions are discussed for a coaxial injector element similar to the SSME preburner element operating with water and air at atmospheric pressure and liquid and gaseous nitrogen at 20 bars.
Document ID
19940018574
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kaltz, T.
(Pennsylvania State Univ. University Park, PA, United States)
Glogowski, M.
(Pennsylvania State Univ. University Park, PA, United States)
Micci, M. M.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Publication Information
Publication: NASA Propulsion Engineering Research Center, Volume 2
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
94N23047
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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