Understanding valve behavior will aid testing of rocket components at Stennis Space Center. The authors of this viewgraph presentation have developed a computational model for a cryogenic liquid control valve, and a gas pressure regulator valve. The model is a compressible/incompressible pressure-based FDNS code from Marshall Space Flight Center (MSFC). It is a k-epsilon turbulence model with wall functions.


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    Title :

    Progress in Valve Modeling at Stennis Space Center


    Contributors:

    Conference:

    14th Annual Symposium on Propulsion ; 2002 ; State College, PA, United States


    Publication date :

    2003-12-04


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




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