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    Thermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004::page 637
    Author:
    Dilip Prasad
    ,
    Jinzhang Feng
    DOI: 10.1115/1.1791288
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical method is developed for transient linear analysis of quasi-one-dimensional thermoacoustic systems, with emphasis on stability properties. This approach incorporates the effects of mean flow variation as well as self-excited sources such as the unsteady heat release across a flame. Working in the frequency domain, the perturbation field is represented as a superposition of local wave modes, which enables the linearized equations to be integrated in space. The problem formulation is completed by specifying appropriate boundary conditions. Here, we consider impedance boundary conditions as well as those relevant to choked and shocked flows. For choked flows, the boundary condition follows from the requirement that perturbations remain regular at the sonic point, while the boundary conditions applicable at a normal shock are obtained from the shock jump conditions. The numerical implementation of the proposed formulation is described for the system eigenvalue problem, where the natural modes are sought. The scheme is validated by comparison with analytical and numerical solutions.
    keyword(s): Flow (Dynamics) , Eigenvalues , Equations , Boundary-value problems , Stability AND Shock (Mechanics) ,
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      Thermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/130965
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    contributor authorDilip Prasad
    contributor authorJinzhang Feng
    date accessioned2017-05-09T00:14:39Z
    date available2017-05-09T00:14:39Z
    date copyrightOctober, 2004
    date issued2004
    identifier issn0889-504X
    identifier otherJOTUEI-28715#637_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130965
    description abstractA numerical method is developed for transient linear analysis of quasi-one-dimensional thermoacoustic systems, with emphasis on stability properties. This approach incorporates the effects of mean flow variation as well as self-excited sources such as the unsteady heat release across a flame. Working in the frequency domain, the perturbation field is represented as a superposition of local wave modes, which enables the linearized equations to be integrated in space. The problem formulation is completed by specifying appropriate boundary conditions. Here, we consider impedance boundary conditions as well as those relevant to choked and shocked flows. For choked flows, the boundary condition follows from the requirement that perturbations remain regular at the sonic point, while the boundary conditions applicable at a normal shock are obtained from the shock jump conditions. The numerical implementation of the proposed formulation is described for the system eigenvalue problem, where the natural modes are sought. The scheme is validated by comparison with analytical and numerical solutions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermoacoustic Stability of Quasi-One-Dimensional Flows–Part I: Analytical and Numerical Formulation
    typeJournal Paper
    journal volume126
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1791288
    journal fristpage637
    journal lastpage644
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsEigenvalues
    keywordsEquations
    keywordsBoundary-value problems
    keywordsStability AND Shock (Mechanics)
    treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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