Tests of drag due to Wright Whirlwind engine, mounted on cabin-type airplane, made in 20-ft. N.A.C.A. Propeller Research Tunnel; drag obtained with three different types of exhaust stacks; drag due to engine found to be 85 lb. at 100 m.p.h. with individual stacks, and 83 lb. at 100 m.p.h. with each of collector rings.
The drag of A J-5 air-cooled engine
Nat. Advisory Committee Aeronautics -- Tech. Notes
1928
4 pages
5 Figs.
Report
English
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The drag of a J-5 radial air-cooled engine
Engineering Index Backfile | 1929
|The drag of a J 5 radial air cooled engine
SLUB | 1928
|Engineering Index Backfile | 1940
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