Theoretical performance of propulsion systems having high combustion temperatures can be calculated on assumption that chemical equilibrium exists among products of reaction; rapidly convergent successive approximation process is presented that simultaneously determines both composition and temperature resulting from chemical reaction.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    General method for computation of equilibrium composition and temperature of chemical reactions


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Hull, V.N. (Autor:in) / Morrell, V.E. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    47 pages


    Anmerkungen:

    Tables


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :