The recent worldwide interest in developing ramjet engines has motivated this preliminary study of the ramjet thermodynamic cycle. Results show that for fixed flight conditions (altitude, flight Mach number and thrust) there is an optimum combustor temperature which furnishes a minimum fuel consumption.


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    Title :

    Estudo Termodinamico de Estato-Reatores (Thermodynamic Study of Ramjet Engines)


    Contributors:

    Publication date :

    1986


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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