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Unformatted text preview: 2 6, 1 931, p p . 5 31-541, i llus., diagrs. A t t his time Taylor
w as chief engineer a t W right Aero.
D IETRICH, OTTO, a nd LEHR, ERNST. D as Dehnungslinienverfahren ein Mittel zur B estimmung d er fur d ie B ruchsichereit b ei W echselbeanspruchung massgebenden
S pannungsverteilung. £eitschrift des Vereines Deutscher Ingenieure, v ol. 76, no. 41
( October 8, 1932), pp. 973-982, illus. This article introduced the very important
m ethod of e xploring stresses in e ngine parts by the b rittle-lacquer technique. I t
h as had a p rofoundly beneficial effect o n e ngine development since that time.
L OWES, JOSEPH E . T he Pratt & W hitney twin Wasp J r . engine. Journal of the American
Society of Naval Engineers, v ol. 44, no. 3 ( August 1932), pp. 371-373.
A NGLE, GLENN D . Developments i n h igh-powered aircraft engines. Aero Digest, v ol. 23,
n o. 4 ( October 1933), p p . 4 1-44, a nd n o. 5 ( November 1933), p p . 4 6-47, illus.
E mphasis is u pon liquid-cooled engines.
C omparison of r ecent European a nd A merican military aircraft engines. Interavia,
n o. 41 (August 24, 1933), pp. 1-2, and no. 42 (August 28, 1933), p p. 1-2.
F EDDEN, A . H . R . N ext decade's aero engines will b e a dvanced b ut not r adical. SAE
Transactions, v ol. 28, 1933, pp. 3 77-401, i llus., drgs., diagrs. Draws heavily upon
Bristol's experience. Fedden w as chief engineer for the e ngines of the B ristol
A eroplane Company.
H igh-output engines: A B ritish point of v iew a nd an A merican one. Aviation, v ol. 3 2,
n o. 10 ( October 1933), pp. 321-323.
H ILL, HENRY C . 4 00-hour endurance test of the W right Whirlwind R - 7 6 0 E - 1 . Aero
Digest, v ol. 23, no. 3 ( September 1933), pp. 5 0-51.
P ratt & W hitney t wo-row e ngine development. Aviation Engineering, v ol. 8, n o. 4 ( April
1933), p p. 17-18, 27, illus.
T AYLOR, E . S. R adial engines: Their power and frontal area. Aviation, v ol. 32, no. 7
( July 1933), pp. 201-202. 108 T he Hispano-Suiza aero engines. Interavia, n o. 166 (November 8, 1934), pp. 1-6.
T AYLOR, C . F AYETTE. P ower plants in 1933. Aviation, v ol. 34, no. 1 (January 1934),
p p. 1 9-20.
See also u nder History and Technology ( DAVY a nd R ICHARDS, 1930). Engines 1935-1939
P ratt & Whitney E Hornet, 750 h.p. engine. Aero Digest, v ol. 26, no. 1 (January 1935),
p p. 4 2-43.
C HATFIELD, CHARLES H . Pratt & Whitney's development of the two-row radial aircraft engine. Aero Digest, v ol. 26, no. 4 (April 1935), pp. 32-34, illus.
W right series F-50 Cyclone engines. Aero Digest, v ol. 26, no. 6 (June 1935), pp. 30, 32,
36, i llus.
Bristol Pegasus Engine. Automobile Engineer, v ol. 26, no. 346 (June 1936), pp. 221-224.
B ristol poppet-valve engine with aluminum heads. Successor to the "Jupiter."
L URENBAUM, K ARL. V ibration of crankshaft-propeller Systems. SAE Transactions, v ol.
3 1, 1936, pp. 469-472.
T AYLOR, E . S. Eliminating crankshaft torsional vibration in radial aircraft engines.
SAE Transactions, v ol. 3 1, 193...
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