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Effect of air-fuel ratio on detonation in gasoline engines (1938)
NASA Technical Reports Server (NTRS) · leaf 18
H.A,C.A. Technical Memorandum Ho. 853 Jigs. 11,12 ...... ... - i Temperature of cooling liquid Curves 68 °C. Exhaust valyes A,B and C Points x 96 °C. Intake " X " I Points © 58 °C. Plugs in positions 1 and 3 … 1.0 1.2 1.4 1.6 _ . - S^iial-ai(r--ra±io r * r ?igure 11. 9 d 8 S co CD •S5 ! ^4 0.2 0.6 1.0 1.4 1.8 2.2 2.6 eft Fuel-ai-r ratio figure 12.NASA Technical Reports Server (NTRS)
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