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    Lumped Capacitance and Three Dimensional Computational Fluid Dynamics Conjugate Heat Transfer Modeling of an Automotive Turbocharger

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 009::page 92602
    Author:
    Burke, R. D.
    ,
    Copeland, C. D.
    ,
    Duda, T.
    ,
    Rayes
    DOI: 10.1115/1.4032663
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Onedimensional waveaction engine models have become an essential tool within engine development including stages of component selection, understanding system interactions, and control strategy development. Simple turbocharger models are seen as a weak link in the accuracy of these simulation tools, and advanced models have been proposed to account for phenomena including heat transfer. In order to run within a full engine code, these models are necessarily simple in structure yet are required to describe a highly complex 3D problem. This paper aims to assess the validity of one of the key assumptions in simple heat transfer models, namely, that the heat transfer between the compressor casing and intake air occurs only after the compression process. Initially, a sensitivity study was conducted on a simple lumped capacity thermal model of a turbocharger. A new partition parameter was introduced خ±A, which divides the internal wetted area of the compressor housing into preand postcompression. The sensitivity of heat fluxes to خ±A was quantified with respect to the sensitivity to turbine inlet temperature (TIT). At low speeds, the TIT was the dominant effect on compressor efficiency, whereas at high speed خ±A had a similar influence to TIT. However, modeling of the conduction within the compressor housing using an additional thermal resistance caused changes in heat flows of less than 10%. Threedimensional computational fluid dynamics (CFD) analysis was undertaken using a number of cases approximating different values of خ±A. It was seen that when considering a case similar to خ±A = 0, meaning that heat transfer on the compressor side is considered to occur only after the compression process, significant temperature could build up in the impeller area of the compressor housing, indicating the importance of the precompression heat path. The 3D simulation was used to estimate a realistic value for خ±A which was suggested to be between 0.15 and 0.3. Using a value of this magnitude in the lumped capacitance model showed that at low speed there would be less than 1% point effect on apparent efficiency which would be negligible compared to the 8% point seen as a result of TIT. In contrast, at high speeds, the impact of خ±A was similar to that of TIT, both leading to approximately 1% point apparent efficiency error.
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      Lumped Capacitance and Three Dimensional Computational Fluid Dynamics Conjugate Heat Transfer Modeling of an Automotive Turbocharger

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    contributor authorBurke, R. D.
    contributor authorCopeland, C. D.
    contributor authorDuda, T.
    contributor authorRayes
    date accessioned2017-05-09T01:28:42Z
    date available2017-05-09T01:28:42Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_09_092602.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161153
    description abstractOnedimensional waveaction engine models have become an essential tool within engine development including stages of component selection, understanding system interactions, and control strategy development. Simple turbocharger models are seen as a weak link in the accuracy of these simulation tools, and advanced models have been proposed to account for phenomena including heat transfer. In order to run within a full engine code, these models are necessarily simple in structure yet are required to describe a highly complex 3D problem. This paper aims to assess the validity of one of the key assumptions in simple heat transfer models, namely, that the heat transfer between the compressor casing and intake air occurs only after the compression process. Initially, a sensitivity study was conducted on a simple lumped capacity thermal model of a turbocharger. A new partition parameter was introduced خ±A, which divides the internal wetted area of the compressor housing into preand postcompression. The sensitivity of heat fluxes to خ±A was quantified with respect to the sensitivity to turbine inlet temperature (TIT). At low speeds, the TIT was the dominant effect on compressor efficiency, whereas at high speed خ±A had a similar influence to TIT. However, modeling of the conduction within the compressor housing using an additional thermal resistance caused changes in heat flows of less than 10%. Threedimensional computational fluid dynamics (CFD) analysis was undertaken using a number of cases approximating different values of خ±A. It was seen that when considering a case similar to خ±A = 0, meaning that heat transfer on the compressor side is considered to occur only after the compression process, significant temperature could build up in the impeller area of the compressor housing, indicating the importance of the precompression heat path. The 3D simulation was used to estimate a realistic value for خ±A which was suggested to be between 0.15 and 0.3. Using a value of this magnitude in the lumped capacitance model showed that at low speed there would be less than 1% point effect on apparent efficiency which would be negligible compared to the 8% point seen as a result of TIT. In contrast, at high speeds, the impact of خ±A was similar to that of TIT, both leading to approximately 1% point apparent efficiency error.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLumped Capacitance and Three Dimensional Computational Fluid Dynamics Conjugate Heat Transfer Modeling of an Automotive Turbocharger
    typeJournal Paper
    journal volume138
    journal issue9
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4032663
    journal fristpage92602
    journal lastpage92602
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 009
    contenttypeFulltext
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