A Preliminary Study of Fuel Injection and Compression Ignition as Applied to an Aircraft Engine Cylinder (1927)
NASA Technical Reports Server (NTRS) · leaf 17
. M., for nozzle orifices 0.012, 0.014, 0.018, and 0.022 inch in diameter, for opening pressures of 2,200, 3,200, and 5,000 pounds per square inch and for varying fuel quantities. The results obtained with three sizes of nozzle orifice are shown on Figures 16, 17, and 18. Figure 19 is a cross plot… … Stroke, inches Stroke, inches -Lipped nozzle with 0.018 inch diameter . —Lipped nozzle with 0.011- Fig. 16.—Lipped nozzle with 0.012-inch diame- hole inch diameter hole ter hole Characteristics of spring actuated fuel pump. Effect of pump stroke and valve opening pressure on lag and interval of…
NASA Technical Reports Server (NTRS)
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