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 Aviation Eng., vol. 10, no. 2, Oct. 1929, p. 44, 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
West. Flying
Western Flying ; 6 , n 4
1929
1 Fig.
Article (Journal)
English
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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