Some Effects of Injection Advance Angle, Engine-Jacket Temperature, and Speed on Combustion in a Compression-Ignition Engine (1936)
NASA Technical Reports Server (NTRS) · leaf 15
Figure 17.—Effect of injection advance angle on flame formation. Engine speed, 1,500 r. p. m.; engine-jacket temperature, 150° F.; fuel quantity, 0.00025 lb.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
