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    Uncertainty Quantification and Conjugate Heat Transfer: A Stochastic Analysis

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003::page 31014
    Author:
    Montomoli, F.
    ,
    D’Ammaro, A.
    ,
    Uchida, S.
    DOI: 10.1115/1.4007516
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Conjugate heat transfer is gaining acceptance for predicting the thermal loading in high pressure nozzles. Despite the accuracy nowadays of numerical solvers, it is not clear how to include the uncertainties associated to the turbulence level, the temperature distribution, or the thermal barrier coating thickness in the numerical simulations. All these parameters are stochastic even if their value is commonly assumed to be deterministic. For the first time, in this work a stochastic analysis is used to predict the metal temperature in a real highpressure nozzle. The domain simulated is the high pressure nozzle of an Ftype Mitsubishi Heavy Industries gas turbine. The complete coolant system is included: impingement, film, and trailing edge cooling. The stochastic variations are included by coupling uncertainty quantification methods and conjugate heat transfer. Two uncertainty quantification methods have been compared: a probabilistic collocation method (PCM) and a stochastic collocation method (SCM). The stochastic distribution of thermal barrier coating thickness, used in the simulations, has been measured at the midspan. A Gaussian distribution for the turbulence intensity and hot core location has been assumed. By using PCM and SCM, the probability to obtain a specific metal temperature at midspan is evaluated. The two methods predict the same distribution of temperature with a maximum difference of 0.6%, and the results are compared with the experimental data measured in the real engine. The experimental data are inside the uncertainty band associated to the CFD predictions. This work shows that one of the most important parameters affecting the metal temperature uncertainty is the pitchwise location of the hot core. Assuming a probability distribution for this location, with a standard deviation of 1.7 deg, the metal temperature at midspan can change up to 30%. The impact of turbulence level and thermal barrier coating thickness is 1 order of magnitude less important.
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      Uncertainty Quantification and Conjugate Heat Transfer: A Stochastic Analysis

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    http://yetl.yabesh.ir/yetl1/handle/yetl/153335
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    contributor authorMontomoli, F.
    contributor authorD’Ammaro, A.
    contributor authorUchida, S.
    date accessioned2017-05-09T01:03:09Z
    date available2017-05-09T01:03:09Z
    date issued2013
    identifier issn0889-504X
    identifier otherturb_135_3_031014.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153335
    description abstractConjugate heat transfer is gaining acceptance for predicting the thermal loading in high pressure nozzles. Despite the accuracy nowadays of numerical solvers, it is not clear how to include the uncertainties associated to the turbulence level, the temperature distribution, or the thermal barrier coating thickness in the numerical simulations. All these parameters are stochastic even if their value is commonly assumed to be deterministic. For the first time, in this work a stochastic analysis is used to predict the metal temperature in a real highpressure nozzle. The domain simulated is the high pressure nozzle of an Ftype Mitsubishi Heavy Industries gas turbine. The complete coolant system is included: impingement, film, and trailing edge cooling. The stochastic variations are included by coupling uncertainty quantification methods and conjugate heat transfer. Two uncertainty quantification methods have been compared: a probabilistic collocation method (PCM) and a stochastic collocation method (SCM). The stochastic distribution of thermal barrier coating thickness, used in the simulations, has been measured at the midspan. A Gaussian distribution for the turbulence intensity and hot core location has been assumed. By using PCM and SCM, the probability to obtain a specific metal temperature at midspan is evaluated. The two methods predict the same distribution of temperature with a maximum difference of 0.6%, and the results are compared with the experimental data measured in the real engine. The experimental data are inside the uncertainty band associated to the CFD predictions. This work shows that one of the most important parameters affecting the metal temperature uncertainty is the pitchwise location of the hot core. Assuming a probability distribution for this location, with a standard deviation of 1.7 deg, the metal temperature at midspan can change up to 30%. The impact of turbulence level and thermal barrier coating thickness is 1 order of magnitude less important.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUncertainty Quantification and Conjugate Heat Transfer: A Stochastic Analysis
    typeJournal Paper
    journal volume135
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4007516
    journal fristpage31014
    journal lastpage31014
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 003
    contenttypeFulltext
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