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    Kinetics of Jet Fuel Combustion Over Extended Conditions: Experimental and Modeling

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002::page 394
    Author:
    Philippe Dagaut
    DOI: 10.1115/1.2364196
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The oxidation of kerosene (Jet-A1) has been studied experimentally in a jet-stirred reactor at 1 to 40atm and constant residence time, over the high temperature range 800–1300K, and for variable equivalence ratio 0.5<φ<2. Concentration profiles of reactants, stable intermediates, and final products have been obtained by probe sampling followed by on-line and off-line GC analyses. The oxidation of kerosene in these conditions was modeled using a detailed kinetic reaction mechanism (209 species and 1673 reactions, most of them reversible). In the kinetic modeling, kerosene was represented by four surrogate model fuels: 100% n-decane, n-decane-n-propylbenzene (74%∕26%mole), n-decane-n-propylcyclohexane (74%∕26%mole), and n-decane-n-propylbenzene-n-propylcyclohexane (74%∕15%∕11%mole). The three-component model fuel was the most appropriate for simulating the JSR experiments. It was also successfully used to simulate the structure of a fuel-rich premixed kerosene-oxygen-nitrogen flame and ignition delays taken from the literature.
    keyword(s): Fuels , Modeling , oxidation , Oxygen , Nitrogen AND Flames ,
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      Kinetics of Jet Fuel Combustion Over Extended Conditions: Experimental and Modeling

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135736
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    contributor authorPhilippe Dagaut
    date accessioned2017-05-09T00:23:43Z
    date available2017-05-09T00:23:43Z
    date copyrightApril, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26949#394_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135736
    description abstractThe oxidation of kerosene (Jet-A1) has been studied experimentally in a jet-stirred reactor at 1 to 40atm and constant residence time, over the high temperature range 800–1300K, and for variable equivalence ratio 0.5<φ<2. Concentration profiles of reactants, stable intermediates, and final products have been obtained by probe sampling followed by on-line and off-line GC analyses. The oxidation of kerosene in these conditions was modeled using a detailed kinetic reaction mechanism (209 species and 1673 reactions, most of them reversible). In the kinetic modeling, kerosene was represented by four surrogate model fuels: 100% n-decane, n-decane-n-propylbenzene (74%∕26%mole), n-decane-n-propylcyclohexane (74%∕26%mole), and n-decane-n-propylbenzene-n-propylcyclohexane (74%∕15%∕11%mole). The three-component model fuel was the most appropriate for simulating the JSR experiments. It was also successfully used to simulate the structure of a fuel-rich premixed kerosene-oxygen-nitrogen flame and ignition delays taken from the literature.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleKinetics of Jet Fuel Combustion Over Extended Conditions: Experimental and Modeling
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2364196
    journal fristpage394
    journal lastpage403
    identifier eissn0742-4795
    keywordsFuels
    keywordsModeling
    keywordsoxidation
    keywordsOxygen
    keywordsNitrogen AND Flames
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
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