Analysis particularly emphasizes cost of design compromises in operation of engine over range of altitudes and powers; for geared-in turbines, compressor losses were sometimes large and altitude range was restricted; by use of auxiliary propeller, these losses could be reduced.


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    Titel :

    Performance of composite engine consisting of reciprocating spark-ignition engine, blowdown turbine, and steady-flow turbine


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Turner, L.R. (Autor:in) / Noyes, R.N. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    56 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :