NASA NTRS · 19730003058
Analysis of propellant feedline dynamics
Abstract
An analytical model and computer program were developed for studying the disturbances of liquid propellants in engine feedline systems. It was found that the predominant effect of turbulence is to increase the spatial attenuation at low frequencies; at high frequencies the laminar and turbulent frequencies coincide. Recommendations for future work are included.
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Astleford, W. J., Holster, J. L., Gerlach, C. R.. 1972-08-01. Analysis of propellant feedline dynamics. https://ntrs.nasa.gov/citations/19730003058
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