It is pointed out that possible techniques are closely analogous with known solutions of matching high and low pressure ends of mechanical compressor.


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    Title :

    Note on matching supersonic intake to aircraft gas turbine


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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