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Effect of Nozzle Design on Fuel Spray and Flame Formation in a High-Speed Compression-Ignition Engine (1937)
NASA Technical Reports Server (NTRS) · leaf 7
T.C. 10 B.T.C. CRANKSHAFT DEGREES FIGURE 3—Effect of nozzle design on fuel spray and flame formation. Air-fuel ratio, 17; compression ratio, 13.2; speed. 1,500 r. p. in.; jacket temperature, 150° F.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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