Review of development and possibilities of improved designs; data on fuel consumption and weight; air vs. water cooling; supercharging; sleeve-valve performance; exhaust at pressure of 300 lb. per sq. in. can be used in low-pressure cylinder; compression ignition. (See also R. Ricardo. Roy. Aeronautical Soc. -- Jl vol. 34, no. 240, Dec. 1930 pp. 1000-1015, 5 figs; Aeroplane, vol. 38, no. 23, June 4, 1930, pp. 1075-1076, 1078 and 1080, 4 figs.; Engineer, vol. 149, no. 3882, June 6, 1930, pp. 628-630, and editorial comment on pp. 635-636, and Automobile Engr., vol. 20, no. 269, July 1930, pp. 255-259, 5 figs)
The development and progress of the aero engine
Flight
Flight ; 22 , n 23
1930
5 pages
Aufsatz (Zeitschrift)
Englisch
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The development and progress of the aero engine
Engineering Index Backfile | 1930
|The development and progress of the aero engine
Engineering Index Backfile | 1930
|The development and progress of the aero engine
Engineering Index Backfile | 1930
|Emerald Group Publishing | 1932
|Engineering Index Backfile | 1935