YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    A Kriging Surrogate Model for Computing Gas Mixture Equations of State

    Source: Journal of Fluids Engineering:;2019:;volume( 141 ):;issue: 009::page 91301
    Author:
    Ouellet, Frederick
    ,
    Park, Chanyoung
    ,
    Rollin, Bertrand
    ,
    Haftka, Raphael T.
    ,
    Balachandar, S.
    DOI: 10.1115/1.4042890
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Accurate simulation of the complex flow following the detonation of an explosive material is a challenging problem. In these flows, the detonation products of the explosive must be treated as a real gas while the surrounding air is treated as an ideal gas. As the detonation process unfolds and the blast wave moves into the surrounding ambient air, the products of detonation expand outward and interact with the air creating a mixture region. In this region, both of the state equations for air and the products must be satisfied. One of the most accurate, yet computationally expensive, methods to handle this problem is an algorithm that iterates between the equations of state until both pressure and temperature reach an equilibrium inside of a computational cell. Since this mixture region moves and grows over time, this algorithm must be performed millions, or even billions, of times in a typical detonation simulation. As such, these calculations can account for a large percentage of the overall solution time. This work aims to use a kriging surrogate model to replace this process. The iterative method solves a nonlinear system of equations created from the gas mixture density, internal energy, and composition using a Broyden iterative solver to obtain an output pressure and temperature. Kriging is used to produce curve fits which interpolate selected pressures and temperatures from this solver from appropriate ranges of the mixture input quantities. Using a finite volume hydrocode, the performance of the model with respect to the iterative solver is demonstrated in the simulation of a pentaerythritol tetranitrate (PETN) charge detonation. The model's computational speed and accuracy are quantified as a function of the choice of sampling points in order to try optimize the combination as well as to show the benefits of this novel approach.
    • Download: (4.190Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      A Kriging Surrogate Model for Computing Gas Mixture Equations of State

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4258535
    Collections
    • Journal of Fluids Engineering

    Show full item record

    contributor authorOuellet, Frederick
    contributor authorPark, Chanyoung
    contributor authorRollin, Bertrand
    contributor authorHaftka, Raphael T.
    contributor authorBalachandar, S.
    date accessioned2019-09-18T09:04:25Z
    date available2019-09-18T09:04:25Z
    date copyright3/25/2019 12:00:00 AM
    date issued2019
    identifier issn0098-2202
    identifier otherfe_141_09_091301.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4258535
    description abstractAccurate simulation of the complex flow following the detonation of an explosive material is a challenging problem. In these flows, the detonation products of the explosive must be treated as a real gas while the surrounding air is treated as an ideal gas. As the detonation process unfolds and the blast wave moves into the surrounding ambient air, the products of detonation expand outward and interact with the air creating a mixture region. In this region, both of the state equations for air and the products must be satisfied. One of the most accurate, yet computationally expensive, methods to handle this problem is an algorithm that iterates between the equations of state until both pressure and temperature reach an equilibrium inside of a computational cell. Since this mixture region moves and grows over time, this algorithm must be performed millions, or even billions, of times in a typical detonation simulation. As such, these calculations can account for a large percentage of the overall solution time. This work aims to use a kriging surrogate model to replace this process. The iterative method solves a nonlinear system of equations created from the gas mixture density, internal energy, and composition using a Broyden iterative solver to obtain an output pressure and temperature. Kriging is used to produce curve fits which interpolate selected pressures and temperatures from this solver from appropriate ranges of the mixture input quantities. Using a finite volume hydrocode, the performance of the model with respect to the iterative solver is demonstrated in the simulation of a pentaerythritol tetranitrate (PETN) charge detonation. The model's computational speed and accuracy are quantified as a function of the choice of sampling points in order to try optimize the combination as well as to show the benefits of this novel approach.
    publisherAmerican Society of Mechanical Engineers (ASME)
    titleA Kriging Surrogate Model for Computing Gas Mixture Equations of State
    typeJournal Paper
    journal volume141
    journal issue9
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4042890
    journal fristpage91301
    journal lastpage091301-15
    treeJournal of Fluids Engineering:;2019:;volume( 141 ):;issue: 009
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian