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 translation in Nat. Advisory Committee Aeronautics -- Tech. Memo., no. 649, Dec. 1931, 11 pp., 13 figs. on supp. plates)
Liquid cooling of aircraft engines
Versuche mit Heisskuehlung am Flugmotor
1931
6 pages
15 Figs.
Aufsatz (Zeitschrift)
Deutsch
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