Studies of three engine configurations made for flight conditions from sea level static to 600 mph at 40,000 ft; it was concluded that turbine frontal area, stress, and pressure ratio requirements made exhaust area adjustment desirable.


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    Title :

    Compressor and turbine matching considerations in turboprop engines


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1956 Turbine propeller



    Publication date :

    1956


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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