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Liquid cooling of aircraft engines (1931)

NASA Technical Reports Server (NTRS) · leaf 16

An illustration from Liquid cooling of aircraft engines, 1931, leaf 16
N.A.C.A. Technical Memorandum No.649 Figs.12,13 100 Cooling liquid,glycol. •p 0 Arado SCI D 1241 O o 80 u ft Original effective c6 <D radiator area for S 60 water cooling=100jo= 10.93 m2=19 radiator u o -p plates. •H ? 40 • Radiator of new design 0) > •H + Removal of radiator o plates from 'below.… … § 1200 1400 1600 1800 r.p.m. Fig. 13 Mean temperature of liquid reduced to 11°C outside temperature and plotted against engine r.p.m.

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