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 and Aviation Eng v 2 n 8 Aug 1929 p 35-36 1 Fig.)
The Warner Scarab aircraft engine
Aero Digest
Aero Digest ; 14 , n 2
1929
4 Figs.
Aufsatz (Zeitschrift)
Englisch
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The Warner Scarab aircraft engine
Engineering Index Backfile | 1929
The Warner Scarab aircraft engine
Engineering Index Backfile | 1929
Four-place warner super scarab-powered Cessna C34 cabin monoplane
Engineering Index Backfile | 1935
ScaRaB and ERBE Radiation Climatology Resampled
Online Contents | 1999
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