NASA NTRS · 19770012219
Analysis of rocket engine injection combustion processes
Abstract
Mixing methodology improvement for the JANNAF DER and CICM injection/combustion analysis computer programs was accomplished. ZOM plane prediction model development was improved for installation into the new standardized DER computer program. An intra-element mixing model developing approach was recommended for gas/liquid coaxial injection elements for possible future incorporation into the CICM computer program.
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Salmon, J. W., Saltzman, D. H.. 1977-02-01. Analysis of rocket engine injection combustion processes. https://ntrs.nasa.gov/citations/19770012219
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