The two net facilities were installed and operated at their design, or rated conditions. The important feature of both of these facilities is that the ratio of turbine inlet temperature to coolant temperature encountered in high temperature engines can be duplicated at moderate turbine inlet temperature. The limits of the facilities with regard to maximum temperature, maximum pressure, maximum mass flow rate, turbine size, and dynamometer torque-speed characteristics are discussed.


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    Title :

    Description of the warm core turbine facility recently installed at NASA Lewis Research Center


    Contributors:

    Conference:

    Aerospace Congr. ; 1980 ; Los Angeles


    Publication date :

    1980-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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