Description of some of problem areas involved in engine structure of high speed ramjet, intended to propel aircraft at about 5000 mph; phenomenon from which severest practical problems stem is increase in ram temperature with flight speed; methods adopted for cooling engine structure, particularly combustion chamber and nozzle walls, will depend upon type of aircraft and its mission; component performance problems relating to intake, combustor, and exhaust nozzle are considered and research being conducted in these areas is indicated.


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    Title :

    Review of problems and research on components for hypersonic air breathing engines


    Additional title:

    Aircraft Eng


    Contributors:
    Hawkins, R. (author)

    Published in:

    Publication date :

    1966


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English