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p p. 294—303. The Smith 10-cyl 4 00-hp, radial, air-cooled engine.
V INCENT, J . G. The Liberty aircraft engine. SAE Transactions, vol. 14, pt. 1 (1919),
p p. 3 85-432, illus., drgs. in text and large fold-out drg., tab. and graph data.
W ARDROP, G . D OUGLAS. T he Liberty engine. The Aeroplane, v ol. 16, J anuary 29, 1919,
p p. 4 80-482, 499-500; February 5, 1919, pp. 582, 599; and February 12, 1919,
p p. 6 76-678, 680, 697. Illus.
See also u nder History and Technology ( ANGLE, 1 921; D ICKEY, 1968). Under Engines
1920-1924 ( HELLER, 1920). Engines 1930-1934 ( "The Hispano-Suiza Aero Engines," 1934). Also under NACA Reports: 8th, 1923 ( SPARROW). Engines 1920-1924
A BELL, C . F. Airship machinery, past experience and future requirements.
the Royal Aeronautical Society, vol. 24 no. 113 ( May 1920), pp. 250-268. Journal of BAUMAN, A . Progress made in the construction of giant airplanes in Germany during the
w ar. NACA Technical Note, n o. 29, 1920, 11 p p., tab. data. 104 L OENING, G ROVER C . E ngine shape as affecting airplane operation. SAE Transactions,
vol. 15, pt. 1, 1920, pp. 5 77-590, illus., drgs., t ab. and g raph data.
N OACK, W . G. T ests of the D aimler D - I V a e ngine a t a h igh altitude test bench.
NACA Technical Note, n o. 15, 1920, 20 pp., extensive graph a nd tab. d ata.
S CHWAGER, O TTO. D evelopment of G erman aircraft engines. Aviation, vol. 9, O ctober 1,
1920, p p. 1 61-164, a nd O ctober 15, 1920, pp. 1 86-189.
. R ecent efforts a nd e xperiments i n the c onstruction of a viation engines.
Technical Note, n o. 12, 1920, 18 pp., g raph a nd tab. d ata.
C HORLTON, A LAN E . L. A ero engines. Journal of the Royal Society of Arts [ London], v ol.
6 9, n o. 3589 (September 2 , 1921), p p. 6 89-705; n o. 3590 (September 9, 1921),
p p. 7 07-724; a nd no. 3591 ( September 16, 1921), p p. 7 25-740. Well illus., b y
m any fine drawings.
D evelopment of an A merican pursuit engine. Aviation, vol. 11, n o. 26 ( December 2 6,
1921), p p. 7 35-738. T h e H ispano-Suiza as d eveloped under license i n the U .S.A.
H ELLER, A . T h e 300 h.p. B enz aircraft engine. Transl. from ^eitschrift des Vereines
Deutsche Ingenieure ( 1920). NACA Technical Note, n o. 34, 1921, 17 p p. I ncludes
cross-sectional a nd s everal detail drgs.
S PARROW, S. W. H igh thermal efficiency i n a irplane service. NACA Technical Note,
n o. 3 9, 1 921, 7 p p., d rgs.
T ests of the 450 h.p. Bristol Jupiter engine. Aviation, vol. 11, n o. 24 ( December 12,
1921), p p. 6 85-686, graph a nd tab. d ata.
W A R E , M ARSDEN. Effect of the r eversal of air flow upon d ie d ischarge coefficient of
D urley orifices. NACA Technical Note, n o. 40, 1921, 14 pp., d iagrs., graph data.
H ERON, S. D . Air cooled cylinder design. SAE Transactions, vol. 17, p t. 1, 1922, pp.
3 47^130, illus., drgs., graph a nd tab. d ata. Contains history a nd d etail design.
N avy changes i n L iberty motor responsible for i mprovement i n N avy plane operations.
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