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Combustion in a Bomb with a Fuel-Injection System (1935)
NASA Technical Reports Server (NTRS) · leaf 7
h-pressure gage A', motor L'. spark-timing switch F, clamping rings Q, fuel reservoir B', oil bath M\ stirrer G, clutch R. gear pump C\ orifice, 0.020-inch N', synchronous motor H, condenser, 8 microfarad S, heating coil D', phase-changing gears O', thermometer I, contact point T, high-pressure… … Figure 5.—Effect of time interval (T, — 7\) between injection and spark. Initial air temperature, 200° C; initial air pressure, 6.3 atmospheres, absolute; air-fuel ratio, 15.NASA Technical Reports Server (NTRS)
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