The Quiescent-Chamber Type Compression-Ignition Engine (1937)
NASA Technical Reports Server (NTRS) · leaf 17
nder pressure to compres- Figure 21 show s the effect of injection advance angle sion pressure. The engine-operating characteristics, on engine performance. This performance, with the however, were found to be quite different. At a com- K-4 nozzle, is the best obtained with the quiescent pression… … Fuel quantity, Ib./cyc/e Coo/ant temperature (out), °F. Fn.i kk 12. KtYco <»f coolant temperature on engine performance; i. a. a., 21°; nozzle Figure 23. Efleet of coolant temperature on engine-operating eht.ructerit-ties; H-1. i. a. a., 2J°; nozzle H-1. ably aided in scavenging the combusion…
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