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Analysis of propellant feedline dynamicsAn 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.
Document ID
19730020456
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holster, J. L.
(Southwest Research Inst. San Antonio, TX, United States)
Astleford, W. J.
(Southwest Research Inst. San Antonio, TX, United States)
Gerlach, C. R.
(Southwest Research Inst. San Antonio, TX, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-124308
Report Number: NASA-CR-124308
Accession Number
73N29188
Funding Number(s)
PROJECT: SWRI PROJ. 02-2889
CONTRACT_GRANT: NAS8-25919
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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