Details of 4-cylinder vertical air-cooled De Havilland airplane engine; maximum of 100 hp. developed at 2100 r.p.m.; stroke 5 1/16 in. bore 4 1/2 in.; compression ratio 5 to 1; weight 285 lb.; overhead valve gear.
De Havilland gipsy
West. Flying
Western Flying ; 4 , n 12
1928
1 Fig.
Article (Journal)
English
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Engineering Index Backfile | 1938
Engineering Index Backfile | 1938
Engineering Index Backfile | 1938
Engineering Index Backfile | 1938
Engineering Index Backfile | 1938