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Combustion in a High-Speed Compression-Ignition Engine (1933)
NASA Technical Reports Server (NTRS) · leaf 15
14 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 80 40 O 60 80 B.TC T.C. A.T.C. Cronh degrees Figure 19.—Effect of injection advance angle on combustion. Supercharging pressure =8.75 in. Hg. … T.C. A.T.C. B.T.C Cronh degrees Figure 20.—Effect of injection advance angle on combustion. Supercharging pressure=5 in. Hg.NASA Technical Reports Server (NTRS)
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