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; Flight v 50 n 1972 Oct 10 1946 p 386-7; 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
Aircraft Eng
Aircraft Engineering ; 18 , n 213
1946
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1946
Engineering Index Backfile | 1946
Engineering Index Backfile | 1946
Engineering Index Backfile | 1946
Engineering Index Backfile | 1946