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    Surface Fouling in Aviation Fuels: An Isothermal Chemical Study

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002::page 286
    Author:
    E. G. Jones
    ,
    W. J. Balster
    ,
    J. M. Pickard
    DOI: 10.1115/1.2816590
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface fouling in aircraft fuel lines that results from autoxidation of aviation fuel remains a serious and very complicated problem. This area has been studied using two Jet-A fuels, POSF-2827 and POSF-2980. The results of a series of dynamic experiments conducted in a single-pass, tubular heat exchanger operated at very slow flow rates under near-isothermal conditions are reported herein. Such studies, by minimizing complications resulting from fluid dynamics and heat flow, constitute a simpler global approach to the chemistry of fouling. The basis for the selection of experimental test conditions is discussed, and data from measurements of dissolved oxygen and surface deposition as a function of fuel stress duration are presented. The effects of parameters such as reaction temperature, tube diameter, experimental test time, and fuel dopants are considered.
    keyword(s): Fuels , Aviation , Flow (Dynamics) , Heat , Temperature , Measurement , Stress , Heat exchangers , Aircraft , Chemistry , Oxygen AND Fluid dynamics ,
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      Surface Fouling in Aviation Fuels: An Isothermal Chemical Study

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/116936
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorE. G. Jones
    contributor authorW. J. Balster
    contributor authorJ. M. Pickard
    date accessioned2017-05-08T23:50:07Z
    date available2017-05-08T23:50:07Z
    date copyrightApril, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26751#286_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116936
    description abstractSurface fouling in aircraft fuel lines that results from autoxidation of aviation fuel remains a serious and very complicated problem. This area has been studied using two Jet-A fuels, POSF-2827 and POSF-2980. The results of a series of dynamic experiments conducted in a single-pass, tubular heat exchanger operated at very slow flow rates under near-isothermal conditions are reported herein. Such studies, by minimizing complications resulting from fluid dynamics and heat flow, constitute a simpler global approach to the chemistry of fouling. The basis for the selection of experimental test conditions is discussed, and data from measurements of dissolved oxygen and surface deposition as a function of fuel stress duration are presented. The effects of parameters such as reaction temperature, tube diameter, experimental test time, and fuel dopants are considered.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSurface Fouling in Aviation Fuels: An Isothermal Chemical Study
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816590
    journal fristpage286
    journal lastpage291
    identifier eissn0742-4795
    keywordsFuels
    keywordsAviation
    keywordsFlow (Dynamics)
    keywordsHeat
    keywordsTemperature
    keywordsMeasurement
    keywordsStress
    keywordsHeat exchangers
    keywordsAircraft
    keywordsChemistry
    keywordsOxygen AND Fluid dynamics
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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