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    Acoustic Resonances of an Industrial Gas Turbine Combustion System

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 004::page 766
    Author:
    S. Hubbard
    ,
    Research Associate
    ,
    A. P. Dowling
    DOI: 10.1115/1.1370975
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory is developed to describe low-frequency acoustic waves in the complicated diffuser/combustor geometry of a typical industrial gas turbine. This is applied to the RB211-DLE geometry to give predictions for the frequencies of the acoustic resonances at a range of operating conditions. The main resonant frequencies are to be found around 605 Hz (associated with the plenum) and around 461 Hz and 823 Hz (associated with the combustion chamber), as well as one at around 22 Hz (a bulk mode associated with the system as a whole). The stabilizing effects of a Helmholtz resonator, which models damping through nonlinear effects, are included, together with effects of coupled pressure waves in the fuel supply system.
    keyword(s): Fuels , Acoustics , Industrial gases , Waves , Combustion chambers , Combustion systems , Turbines , Oscillations , Pressure , Flow (Dynamics) , Heat , Flames , Frequency , Geometry , Temperature AND Equations ,
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      Acoustic Resonances of an Industrial Gas Turbine Combustion System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/125132
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    contributor authorS. Hubbard
    contributor authorResearch Associate
    contributor authorA. P. Dowling
    date accessioned2017-05-09T00:04:43Z
    date available2017-05-09T00:04:43Z
    date copyrightOctober, 2001
    date issued2001
    identifier issn1528-8919
    identifier otherJETPEZ-26807#766_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125132
    description abstractA theory is developed to describe low-frequency acoustic waves in the complicated diffuser/combustor geometry of a typical industrial gas turbine. This is applied to the RB211-DLE geometry to give predictions for the frequencies of the acoustic resonances at a range of operating conditions. The main resonant frequencies are to be found around 605 Hz (associated with the plenum) and around 461 Hz and 823 Hz (associated with the combustion chamber), as well as one at around 22 Hz (a bulk mode associated with the system as a whole). The stabilizing effects of a Helmholtz resonator, which models damping through nonlinear effects, are included, together with effects of coupled pressure waves in the fuel supply system.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAcoustic Resonances of an Industrial Gas Turbine Combustion System
    typeJournal Paper
    journal volume123
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1370975
    journal fristpage766
    journal lastpage773
    identifier eissn0742-4795
    keywordsFuels
    keywordsAcoustics
    keywordsIndustrial gases
    keywordsWaves
    keywordsCombustion chambers
    keywordsCombustion systems
    keywordsTurbines
    keywordsOscillations
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsHeat
    keywordsFlames
    keywordsFrequency
    keywordsGeometry
    keywordsTemperature AND Equations
    treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 004
    contenttypeFulltext
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