Description of 6-cylinder inverted in-line air-cooled engine; good forward vision is afforded by position of engine in respect to line of thrust; bore 4 1/8 in.; stroke 5 1/2 in.; piston displacement 441 cu. in.; weight 345 lb.; 2 valves per cylinder; underhead camshaft; pressure feed lubrication. (See also West. Flying vol. 6, no. 4, Oct. 1929 pp. 68 and 142, 1 fig; Aero Digest, vol. 15, no. 5, Nov. 1929, p. 148, 4 figs. and Airway Age, vol. 10, no. 12, Dec. 1929, p. 1988, 2 figs)
Curtiss crusader
Aviation Eng
Aviation Engineering ; 10 , n 2
1929
1 Fig.
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1928
Curtiss. New curtiss hawk army pursuit plane
Engineering Index Backfile | 1929