Advantages as exemplified in Proteus 3; difficulties experienced in developing Proteus and ingenious, in many cases, simple manner in which these setbacks were overcome; comparison between performance of turboprop and turbojet engine designed to give 1200 lb thrust at 350 mph and 36,000 ft. From paper before Roy Aeronautical Soc. (See also Aeroplane v 84 n 2179 Apr 24 1953 p 540)


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    Titel :

    Proof of turbo-prop


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Hooker, S.G. (Autor:in)

    Erschienen in:

    Flight ; 63 , n 2311


    Erscheinungsdatum :

    1953


    Format / Umfang :

    581 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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