Details of development of turbine propeller engine; factors which led to present design; turbine consists of axial flow compressor, combined with centrifugal stage and driven by 2-stage turbine; leading data on engine given. See also Engineering Index 1946 p 36. (See also Aeroplane v 71 n 1842 Sept 13 1946 p 307-9; Aircraft Eng v 18 n 213 Nov 1946 p 366-71; Engineering v 162 n 4214 Oct 18 1946 p 367-9, figs on p 372; Mech World v 120 n 3121 Oct 25 1946 p 458-61; Engineer v 182 n 4732 Sept 20 1946 p 258-61)


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    Title :

    Bristol Theseus I


    Additional title:

    Flight


    Published in:

    Flight ; 50 , n 1972


    Publication date :

    1946


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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