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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    Title :

    Transport Aircraft Intake Design


    Contributors:
    J. Leynaert (author)

    Publication date :

    1988


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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