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    Parametric Studies on a Numerical, Nonlinear Pulse Tube Flow

    Source: Journal of Fluids Engineering:;1997:;volume( 119 ):;issue: 004::page 831
    Author:
    C. S. Kirkconnell
    ,
    G. T. Colwell
    DOI: 10.1115/1.2819505
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The need for high reliability, low cost, low vibration cryocoolers, for both military and commercial applications, has spawned and continues to drive the development of pulse tube cryogenic refrigerators. The expander contains no moving parts, yielding the potential for marked improvements in these areas. Though pulse tube refrigeration has been thoroughly studied, more accurate analytic and numerical modeling tools are needed to facilitate the development of thermodynamically efficient pulse tube cryocoolers to meet the needs of the user community. At present, one of the primary areas of modeling uncertainty is in the calculation of the dissipative losses occurring within the pulse tube itself. Toward this end, a numerical model was developed to solve the one-dimensional, nonlinear governing equations for heat and mass flow in a pulse tube. The governing equations are scaled for high-frequency (>60 Hz) pulse lube operation. The resulting system of nonlinear, time-dependent equations was solved directly using the method of lines. The numerical model was verified analytically using a representative set of equations with a known solution. A sensitivity analysis was performed to investigate the influence of different parameters on the solution.
    keyword(s): Flow (Dynamics) , Equations , Computer simulation , Reliability , Equipment and tools , Modeling , Refrigeration , Vibration , Military systems , Sensitivity analysis , Uncertainty AND Heat ,
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      Parametric Studies on a Numerical, Nonlinear Pulse Tube Flow

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    https://yetl.yabesh.ir/yetl1/handle/yetl/118843
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    contributor authorC. S. Kirkconnell
    contributor authorG. T. Colwell
    date accessioned2017-05-08T23:53:44Z
    date available2017-05-08T23:53:44Z
    date copyrightDecember, 1997
    date issued1997
    identifier issn0098-2202
    identifier otherJFEGA4-27123#831_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118843
    description abstractThe need for high reliability, low cost, low vibration cryocoolers, for both military and commercial applications, has spawned and continues to drive the development of pulse tube cryogenic refrigerators. The expander contains no moving parts, yielding the potential for marked improvements in these areas. Though pulse tube refrigeration has been thoroughly studied, more accurate analytic and numerical modeling tools are needed to facilitate the development of thermodynamically efficient pulse tube cryocoolers to meet the needs of the user community. At present, one of the primary areas of modeling uncertainty is in the calculation of the dissipative losses occurring within the pulse tube itself. Toward this end, a numerical model was developed to solve the one-dimensional, nonlinear governing equations for heat and mass flow in a pulse tube. The governing equations are scaled for high-frequency (>60 Hz) pulse lube operation. The resulting system of nonlinear, time-dependent equations was solved directly using the method of lines. The numerical model was verified analytically using a representative set of equations with a known solution. A sensitivity analysis was performed to investigate the influence of different parameters on the solution.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleParametric Studies on a Numerical, Nonlinear Pulse Tube Flow
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2819505
    journal fristpage831
    journal lastpage837
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsEquations
    keywordsComputer simulation
    keywordsReliability
    keywordsEquipment and tools
    keywordsModeling
    keywordsRefrigeration
    keywordsVibration
    keywordsMilitary systems
    keywordsSensitivity analysis
    keywordsUncertainty AND Heat
    treeJournal of Fluids Engineering:;1997:;volume( 119 ):;issue: 004
    contenttypeFulltext
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