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    Investigating Fuel Condensation Processes in Low Temperature Combustion Engines

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 010::page 101506
    Author:
    Qiu, Lu
    ,
    Reitz, Rolf D.
    DOI: 10.1115/1.4030100
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Condensation of gaseous fuel is investigated in a low temperature combustion (LTC) engine fueled with double directinjected diesel and premixed gasoline at two load conditions. Possible condensation is examined by considering real gas effects with the Peng–Robinson (PR) equation of state (EOS) and assuming thermodynamic equilibrium of the two fuels. The simulations show that three representative condensation events are observed. The first two condensations are found in the spray some time after the two direct injections (DI), when the evaporative cooling reduces the local temperature until phase separation occurs. The third condensation event occurs during the late stages of the expansion stroke, during which the continuous expansion sends the local fluid into the twophase region again. Condensation was not found to greatly affect global parameters, such as the average cylinder pressure and temperature mainly because, before the main combustion event, the condensed phase was converted back to the vapor phase due to compression and/or first stage heat release. However, condensed fuel is shown to affect the emission predictions, including engineout particulate matter (PM) and unburned hydrocarbons (UHCs). Specifically, it was shown that the condensed fuel comprised more than 95% of the PM in the low load condition, while its contribution was significantly reduced at the high load condition due to higher temperature and pressure conditions.
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      Investigating Fuel Condensation Processes in Low Temperature Combustion Engines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/158050
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorQiu, Lu
    contributor authorReitz, Rolf D.
    date accessioned2017-05-09T01:18:16Z
    date available2017-05-09T01:18:16Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_10_101506.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158050
    description abstractCondensation of gaseous fuel is investigated in a low temperature combustion (LTC) engine fueled with double directinjected diesel and premixed gasoline at two load conditions. Possible condensation is examined by considering real gas effects with the Peng–Robinson (PR) equation of state (EOS) and assuming thermodynamic equilibrium of the two fuels. The simulations show that three representative condensation events are observed. The first two condensations are found in the spray some time after the two direct injections (DI), when the evaporative cooling reduces the local temperature until phase separation occurs. The third condensation event occurs during the late stages of the expansion stroke, during which the continuous expansion sends the local fluid into the twophase region again. Condensation was not found to greatly affect global parameters, such as the average cylinder pressure and temperature mainly because, before the main combustion event, the condensed phase was converted back to the vapor phase due to compression and/or first stage heat release. However, condensed fuel is shown to affect the emission predictions, including engineout particulate matter (PM) and unburned hydrocarbons (UHCs). Specifically, it was shown that the condensed fuel comprised more than 95% of the PM in the low load condition, while its contribution was significantly reduced at the high load condition due to higher temperature and pressure conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigating Fuel Condensation Processes in Low Temperature Combustion Engines
    typeJournal Paper
    journal volume137
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4030100
    journal fristpage101506
    journal lastpage101506
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 010
    contenttypeFulltext
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