IT is usually supposed that the designer of a gas turbine engine has considerable freedom in choosing the pressures, temperatures and other features. Indeed this apparent flexibility has been claimed as an inherent advantage of the gas turbine, which enables it to be tailor-made for any prescribed duty.


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    Title :

    Pressure Ratios for Aero-Engines


    Subtitle :

    A Note on the Factors Limiting the Choice of Pressure Ratio


    Contributors:


    Publication date :

    1953-12-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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