High pressure heterogeneous combustion systems typically operate trans- or supercritical: Liquid rocket engines; Gas turbine combustors; and/or Diesel engines. Quantitative assessments or validated theories characterizing propellant injection at near and supercritical conditions are currently limited.


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    Title :

    Molecular Dynamics Simulations of Supercritical Jet Mixing


    Contributors:
    M. M. Micci (author) / R. D. Branam (author) / K. F. Ludwig (author)

    Publication date :

    2004


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English