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    Titel :

    Parallel Compressible Solver for Unsteady Turbulent Combustion in Rocket Injectors Using Flamelet Models


    Beteiligte:

    Kongress:

    21st AIAA Computational Fluid Dynamics Conference



    Erscheinungsdatum :

    01.01.2013



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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