Performance of a Fuel-Injection Spark-Ignition Engine Using a Hydrogenated Safety Fuel (1934)
NASA Technical Reports Server (NTRS) · leaf 6
e length of inlet pipe to the point of attachment at D, Inlet B, Location of fuel E, Piston 5.85 c.r the surge tank was 2% feet, but this length was not in jec tion vol ve Ft Location of C, Piston 70 c.r spark plug critical. With a large valve overlap the effect of pressure waves in the exhaust and… … Fi'ii'HK 2. - Fuel-injection valve and nozzle. \4 from 1,250 to 2,200 r.p.m., compression ratios of 5.85 .2 and 7.0, valve timings giving 30° overlap and 130° overlap, and boost pressures up to 6 inches of mercury. 0 A sufficient number of these tests using fuel injection 180 270 360 630 0 90 450…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
