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Mathematical and experimental investigation of heat control and power increase in air-cooled aircraft engines (1929)
NASA Technical Reports Server (NTRS) · leaf 17
i Figs.23, 24, 35 N.A.C.A. Technical Menornnduin No.540 … 100 120 140 160 180 300 1 t=250° Cy 1. di ajii,,iT)m ^'^^^200^ a,Heat dissipation at different T;all temp. b,Kean heat tre^nsmissioia at head.c,Output,hpg. Fig.23 Heat dissipation plotted aga-inst cyl.diani.at different conpression ratios and wall temp.for cyl.like Figs.7-8 forS/d=1.2, 17=180 km/h…NASA Technical Reports Server (NTRS)
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