Details released by D.Napier and Son of "Nomad", oa compression ratio of 31.5:1 and expansion ratio of 24:1 is achieved, leading to fuel consumption in order of 0. 35 lb per bhp-hr; total power developed in gas turbine alone is 2250 hp and in diesel engine alone 2660 hp. See also Engineering Index 1953 p 41. (See also Engineer v 197 n 5127 Apr 30 1954 p 637-640; Engineering v 177 n 4604 Apr 30 1954 p 571-572; Oil Engine and Gas Turbine v 22 n 251 May 1954 p 18-20; Gas and Oil Power v 49 n 587 May 1954 p 101-4; Aviation Week v 60 n 20 May 17 1954 p 30-2, 34; English Elec J v 13 n 7 Sept 1954 p 295-302)


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    Titel :

    Aeronautical compound diesel engine


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Flight ; 65 , n 2362


    Erscheinungsdatum :

    1954


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aeronautical compound diesel engine

    Engineering Index Backfile | 1954


    Aeronautical compound diesel engine

    Engineering Index Backfile | 1954


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    History of the aeronautical engine

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    A new German aeronautical engine

    Hildesheim, Erik | Engineering Index Backfile | 1922