Theoretical and Experimental Study of Ignition Lag and Engine Knock (1939)
NASA Technical Reports Server (NTRS) · leaf 36
19.- Temperature distribution for unburned fuel quota in cylinder under conditions of Figs. 17 Figure and 18 best for a test series starting in the detonating and. terminating in the knock-free /'tone ai r temperature: 80°C fspark ignition: 38° B.T.C. o … Crank angle >3 20 20 10 0 10 Figure 18.- Mixture temperature T versus start m Of Figure 17.-Mixture temperature T versus start of ignition and compression ratio * 00 ignition and initial temperature T ,at at constant initial temperature t^ = 80°C to constant compression ratio ^^6,
NASA Technical Reports Server (NTRS)
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