Present state of art and performance of bypass turbojets; interrelationship between various design parameters and specific fuel consumption is investigated showing that while bypass-ratio for optimal consumption depends on operating flight Mach-number, bypass-pressure-ratio represents compromise between optimal weight and optimal consumption and has marked influence on all other design parameters; operating flight altitude rather than flight Mach number has considerable influence on choice of optimal turbine inlet temperature with respect to consumption.


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    Title :

    Fuel consumption characteristics of bypass turbojets in subsonic flight regime


    Additional title:

    Die Verbrauchscharakteristik von Zweistromstrahltriebwerken im Unterschallbereich


    Contributors:

    Published in:

    Publication date :

    1966


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English