In this chapter, the operation of a basic turbojet engine is described. This is followed by a discussion of the individual components, namely, the compressor, combustor, turbine and the nozzle. This discussion brings out the details of the operation of these components along with important issues related to their operation. A thermodynamic analysis of the operation of the whole engine as well as the components is deferred till Chap. 7.


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    Title :

    The Turbojet Engine


    Contributors:
    Babu, V. (author)

    Published in:

    Fundamentals of Propulsion ; Chapter : 5 ; 61-81


    Publication date :

    2021-08-26


    Size :

    21 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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