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    Forced and Self-Excited Oscillations in Propellant Lines

    Source: Journal of Fluids Engineering:;1969:;volume( 091 ):;issue: 004::page 671
    Author:
    W. Zielke
    ,
    E. B. Wylie
    ,
    R. B. Keller
    DOI: 10.1115/1.3571208
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analytical techniques used to model the dynamics of propellant feed systems of rocket engines are presented as well as experimental results which provide verification. The laboratory hydraulic system, consisting of suction pipe, centrifugal pump, and discharge pipe, provides longitudinal fluid oscillations which are analyzed by use of linear methods employing a distributed parameter representation of the pipes. Of particular interest is the effect of the pump upon pressure oscillations when the pump is operating under cavitating conditions. A self-excited instability caused by the interaction between hydraulic and structural portions of the system is also described.
    keyword(s): Oscillations , Propellants , Pipes , Pumps , Centrifugal pumps , Fluid oscillations , Hydraulic systems , Dynamics (Mechanics) , Pressure , Suction AND Rocket engines ,
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      Forced and Self-Excited Oscillations in Propellant Lines

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/133846
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    • Journal of Fluids Engineering

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    contributor authorW. Zielke
    contributor authorE. B. Wylie
    contributor authorR. B. Keller
    date accessioned2017-05-09T00:20:09Z
    date available2017-05-09T00:20:09Z
    date copyrightDecember, 1969
    date issued1969
    identifier issn0098-2202
    identifier otherJFEGA4-27348#671_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133846
    description abstractAnalytical techniques used to model the dynamics of propellant feed systems of rocket engines are presented as well as experimental results which provide verification. The laboratory hydraulic system, consisting of suction pipe, centrifugal pump, and discharge pipe, provides longitudinal fluid oscillations which are analyzed by use of linear methods employing a distributed parameter representation of the pipes. Of particular interest is the effect of the pump upon pressure oscillations when the pump is operating under cavitating conditions. A self-excited instability caused by the interaction between hydraulic and structural portions of the system is also described.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleForced and Self-Excited Oscillations in Propellant Lines
    typeJournal Paper
    journal volume91
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3571208
    journal fristpage671
    journal lastpage677
    identifier eissn1528-901X
    keywordsOscillations
    keywordsPropellants
    keywordsPipes
    keywordsPumps
    keywordsCentrifugal pumps
    keywordsFluid oscillations
    keywordsHydraulic systems
    keywordsDynamics (Mechanics)
    keywordsPressure
    keywordsSuction AND Rocket engines
    treeJournal of Fluids Engineering:;1969:;volume( 091 ):;issue: 004
    contenttypeFulltext
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