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 11
rning when it is most probably gas movement. The an injection advance angle of 0° shows several areas of afterburning is marked by well-defined regions of incandescence between the main sprays and between both luminous and nonluminous gases and there is a the main and auxiliary sprays, the light… … Figure 14—Effect of injection advance angle on flame formation. Engine speed, 570 r. p. m.; engine-jacket temperature, 150° F.; fuel quantity, 0.00025 lb.; compression ratio, 13.9. A, i. a. a. 0°; B, i. a. a. 10°; C, i. a. a. 20°; S, fuel spray illuminated by flame. (See also fig. 13.) For an…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
