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Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine (1937)
NASA Technical Reports Server (NTRS) · leaf 18
Scavenging-air pressure, in. JHg figure 6.- Effect of scavenging-air pressure on engine performance. Horizontal air-entry angle,60°; vertical air-entry angle,0°.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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