Comparison of 4 different gas turbines incorporating free turbine, as applied to rotary wing aircraft; consideration of ratio of free turbine shaft horsepower to primary gas flow rate, main compressor turbine shaft horsepower, specific fuel consumption, airflow ratio, and duct pressure and temperature; conclusions summarized.


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    Titel :

    Free turbine systems in rotary wing aircraft


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Hrubecky, H.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Free turbine systems in rotary wing aircraft

    Hrubecky, Henry F. | TIBKAT | 1961



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