Subsonic air intake, Mach 2 transport aircraft intake, and Mach 3 are considered. Hypersonic cruise intakes are mentioned. The problem of supersonic intake adaptation to the intermediate flight Mach number range is reviewed. Future multicycle engine design is discussed.


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    Titel :

    Transport Aircraft Intake Design


    Beteiligte:
    J. Leynaert (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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