Details of static radical aircooled 7-cylinder 4-cycle engine developing 122 hp. at 1950 r.p.m.; weight 270 lb.; fuel consumption 6 to 8 gal. per hr.; bore 4.25 in.; stroke 4.25 in.; compression ratio 5.2 to 1; displacement 422 cu. in. (See also Airway Age vol. 10, no. 1, Jan. 1929 pp. 82-83, 2 figs; Aero Digest, vol. 14, no. 2, Feb. 1929, pp. 114 and 116, 4 figs.)
The Warner Scarab aircraft engine
Aviation Eng
Aviation Engineering ; 2 , n 8
1929
2 pages
1 Fig.
Article (Journal)
English
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The Warner Scarab aircraft engine
Engineering Index Backfile | 1929
The Warner Scarab aircraft engine
Engineering Index Backfile | 1929
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