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.


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Hull, V.N. (author) / Morrell, V.E. (author)


    Publication date :

    1950


    Size :

    47 pages


    Remarks:

    Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :