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)
Bristol Theseus I
Flight
Flight ; 50 , n 1972
1946
2 pages
Article (Journal)
English
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Notes on the Bristol Theseus Heat-Exchanger Propeller Turbine
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