Mathematical and experimental investigation of heat control and power increase in air-cooled aircraft engines (1929)
NASA Technical Reports Server (NTRS) · leaf 16
N.A.CA. Teclinical Keniorajidvu.; Ko.540 Figs.19,20,21,32 … 1200 800 400 0 40 80 '^c/.[kcal/m2n°c] Vm/s Fig. 19 Specifio heat dissipp.tion plotted against mean tenporature and air velocity for various cylinder diameters .L07:er group of curves is for cylinders siio^n in Figs.3-4,upper group for cylinders in Figs.7-3. .a ( a, Q=226700 kcal/m^h d, iSOnirn b,…
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