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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    Titel :

    Pressure Ratios for Aero-Engines


    Untertitel :

    A Note on the Factors Limiting the Choice of Pressure Ratio


    Beteiligte:


    Erscheinungsdatum :

    01.12.1953


    Format / Umfang :

    1 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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