NASA NTRS · 19730020456
Analysis of propellant feedline dynamics
Abstract
An analytical model and corresponding computer program for studying disturbances of liquid propellants in typical engine feedline systems were developed. The model includes the effects of steady turbulent mean flow, the influence of distributed compliances, the effects of local compliances, and various factors causing structural-hydraulic coupling. The computer program was set up such that the amplitude and phase of the terminal pressure/input excitation is calculated over any desired frequency range for an arbitrary assembly of various feedline components. A user's manual is included.
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Holster, J. L., Astleford, W. J., Gerlach, C. R.. 1973-05-01. Analysis of propellant feedline dynamics. https://ntrs.nasa.gov/citations/19730020456
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