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Effect of Propellant Feed System Coupling and Hydraulic Parameters on Analysis of ChuggingA digital distributed parameter model was used to study the effects of propellant-feed- system coupling and various hydraulic parameters on the analytical prediction of chugging instabilities. Coupling between the combustion chamber and feed system was controlled by varying the compliance of the injector-dome region. The coupling with the feed system above the pump was varied by changing the amount of cavitation compliance at the pump inlet. The stability limits and chugging frequencies proved to be strongly dependent on the degree of feed-system coupling. The maximum stability condition occurred with intermediate coupling. Under conditions of a high degree of feed-system-combustor coupling, the stability limits and chugging frequencies were primarily dependent on the feed-system characteristics; the responses were characterized by beating patterns. For the system analyzed, the pump suction line had little effect on the stability limits or chugging frequencies. Beating, present under the condition of near zero injector -dome compliance, was eliminated when the suction line was decoupled by employing a sufficiently high value of pump-inlet compliance. Under conditions of maximum feed-system coupling, the magnitude and distribution of line losses in the discharge line had a significant effect on the stability limits but had negligible effect on the chugging frequency and beating characteristics. Also, the length of the discharge line greatly affected the stability limits, chugging frequency, and beating characteristics. The length of the suction line, however, had little effect on the stability limits and chugging frequency but did influence the beating pattern. A resistive-shunt device attached to the pump discharge line to suppress chugging was investigated. The analysis showed that the device was effective under conditions of high feed-system coupling.
Document ID
19670014466
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Wood, Don J.
(Kentucky Univ. Lexington, KY, United States)
Dorsch, Robert G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Propellants
Report/Patent Number
NASA-TN-D-3896
E-3589
Report Number: NASA-TN-D-3896
Report Number: E-3589
Accession Number
67N23795
Funding Number(s)
CONTRACT_GRANT: 128-31-06-09-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CHUGGING
LIQUID PROPELLANT
FEED SYSTEM
COUPLING
PREDICTION THEORY
HYDRAULIC SYSTEM
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