Charts presented apply to processes in which final mixture is leaner than stoichiometric and are exact below those temperatures at which dissociation becomes important; need arises in performance analysis of aircraft gas turbine engines when diluents or refrigerants are used to augment thrust or power of engine. (25¢)


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    Title :

    Constant-pressure combustion on charts including effects of diluent addition


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Turner, L.R. (author) / Bogart, D. (author)


    Publication date :

    1949


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :