At 293 deg. fahr. mean temperature of cooling liquid, requisite effective radiator area per horsepower is reduced from original 0.04 to 0.011 sq. m. per hp. (See also Zeit. fuer Flugtechnik und Motorluftschiffahrt, vol. 22, no. 18, Sept. 28, 1931, pp. 541-546, 15 figs.)
Liquid cooling of aircraft engines
Versuche mit Heisskuehlung am Flugmotor
1931
11 pages
13 Figs., Supp plates
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Liquid cooling of aircraft engines
Engineering Index Backfile | 1931
|Liquid cooling of aircraft engines
TIBKAT | 1931
|The evaporative cooling of aircraft engines
Engineering Index Backfile | 1925
|Cooling characteristics of submerged light aircraft engines
Engineering Index Backfile | 1941
An improved cooling system for aircraft engines
Engineering Index Backfile | 1929
|