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A Preliminary Motion-picture Study of Combustion in a Compression-ignition Engine (1934)
NASA Technical Reports Server (NTRS) · leaf 12
70' 60' SO" 40' SO' A.TC. rc. Injeciion Ad i/a nee Angle O* B.TC. 1-3 CD … Injeciion Advance Angle 20" B.TC. CD Engine coolant temperature, 150 ^F. Figure 2.- Effect of Engine speed, 570 r.p.m. injection advance angle on flame spread and on pressure rise. 20*AJ.C. /Q' T.C. 10' BT.C. CO Injection Advance Angle ^O" B.TC.NASA Technical Reports Server (NTRS)
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