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    Real Gas Effects for Compressible Nozzle Flows

    Source: Journal of Fluids Engineering:;1993:;volume( 115 ):;issue: 001::page 115
    Author:
    D. Drikakis
    ,
    S. Tsangaris
    DOI: 10.1115/1.2910092
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Numerical simulation of compressible nozzle flows of real gas with or without the addition of heat is presented. A generalized real gas method, using an upwind scheme and curvilinear coordinates, is applied to solve the unsteady compressible Euler equations in axisymmetric form. The present method is an extension of a previous 2D method, which was developed to solve the problem for a gas having the general equation of state in the form p = p(ρ, i). In the present work the method is generalized for an arbitrary P-V-T equation of state introducing an iterative procedure for the determination of the temperature from the specific internal energy and the flow variables. The solution procedure is applied for the study of real gas effects in an axisymmetric nozzle flow.
    keyword(s): Flow (Dynamics) , Nozzles , Equations of state , Equations , Heat , Temperature , Computer simulation AND Internal energy (Physics) ,
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      Real Gas Effects for Compressible Nozzle Flows

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112183
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    contributor authorD. Drikakis
    contributor authorS. Tsangaris
    date accessioned2017-05-08T23:41:45Z
    date available2017-05-08T23:41:45Z
    date copyrightMarch, 1993
    date issued1993
    identifier issn0098-2202
    identifier otherJFEGA4-27073#115_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112183
    description abstractNumerical simulation of compressible nozzle flows of real gas with or without the addition of heat is presented. A generalized real gas method, using an upwind scheme and curvilinear coordinates, is applied to solve the unsteady compressible Euler equations in axisymmetric form. The present method is an extension of a previous 2D method, which was developed to solve the problem for a gas having the general equation of state in the form p = p(ρ, i). In the present work the method is generalized for an arbitrary P-V-T equation of state introducing an iterative procedure for the determination of the temperature from the specific internal energy and the flow variables. The solution procedure is applied for the study of real gas effects in an axisymmetric nozzle flow.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleReal Gas Effects for Compressible Nozzle Flows
    typeJournal Paper
    journal volume115
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2910092
    journal fristpage115
    journal lastpage120
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsNozzles
    keywordsEquations of state
    keywordsEquations
    keywordsHeat
    keywordsTemperature
    keywordsComputer simulation AND Internal energy (Physics)
    treeJournal of Fluids Engineering:;1993:;volume( 115 ):;issue: 001
    contenttypeFulltext
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