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6.3.1: Turbojets

  • Page ID
    78144
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    截屏2022-01-21 下午9.13.34.png
    Figure 6.12: Turbojet with centrifugal compressor.

    截屏2022-01-21 下午9.14.26.png
    Figure 6.13: Turbojet with axial compressor.

    A turbojet is basically what has been already exposed in Section 6.2. It is composed by an inlet, a compressor, a combustion chamber, a turbine, and a nozzle. The reader is referred back to Figure 6.2 as illustration. As already mentioned, there are two main types of turbojets depending on the type of compressor: axial or centrifugal. Figures 6.12-6.13 show schematic and real jet engines with centrifugal and axial flow, respectively.


    6.3.1: Turbojets is shared under a CC BY-SA 3.0 license and was authored, remixed, and/or curated by Manuel Soler Arnedo via source content that was edited to conform to the style and standards of the LibreTexts platform; a detailed edit history is available upon request.

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