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; Aviation Eng., vol. 10, no. 2, Oct. 1929, p. 44, 1 fig.; Airway Age, vol. 10, no. 12, Dec. 1929, p. 1988, 2 figs)
Curtiss crusader
Aero Digest
Aero Digest ; 15 , n 5
1929
4 Figs.
Article (Journal)
English
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Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1929
Engineering Index Backfile | 1930
Engineering Index Backfile | 1945
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