Experiments on self-ignition of liquid fuels (1926)
NASA Technical Reports Server (NTRS) · leaf 31
Figs.13 & 13. N.A.O.A. Technical Memorandum Ho.391 12 1300 10 1000 o o 8to 800 50 S CO o A = Range for 600 Diesel CO engines. 400 273 SOO 6 8 10 13 Air density 7 nr Fig.13 Self-ignition temperature plotted against air density -47°-37° A=C ornpr e s s i on. -497 /-33°-15°-5° B=3xpansion. … =Density 7 -90° -60° '-So0 0° ~~!%P 60° 90° =330° N- , , .Crank ang^e , , , , =7.5 atm. 0 -.04 -".03 0.03 .04 s = 3.75 kg. P Time Q=7k=n.r|;f- Fig.13' Ignition phenomena in a mechanical - injection engine Trith variable injection R= timing. S= Stroke, 450m.ii (17.73in.), bore, 380mm (11.03 in.) T=…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
